Jaxusism
19-12-2003, 22:52
Welcome To JaxForce, Jaxusism & Geforce4's Storefront!
NOTE : Armacor has now joined up with JF in a sorta I supply him he supply my customer sorta thing!
For Sale :
GUNS
XR-1 (X-Rifle)
http://defence-data.com/dsei99/sar21.jpg
Type : Assault Rifle
Manufacterer : JaxusismCorp
Cartridge - 5.56mm
Length - look pic
Weight - light
Barrel - look pic
Magazine - 40 rounds
Rate of Fire - 950rds/min
Muzzle Velocity - 985m/sec
Effective Range - About 1000 yards
Comes with an Attachable 40mm M203 grenade launcher for +$200
Scope with Zoom capabilities for, well, a long range.
Cost : $1,400 + 200 for Attachable Grenade Launcher
Extremely light and a pretty nice size, this assault rifle, the XR-1, spreads 950 rounds a minute. Its range goes about 1000 yards. The scope has zooming capabilities for a long range. And, for 200 extra, you get the attachable 40mm M203 grenade launcher. Buy yours today!
XR-2 (X-Rifle)
NOTE : PIC IS XR-1!! NOT XR-2!!!
http://defence-data.com/dsei99/sar21.jpg
Well, here it is, the XR-2, probably the best rifle ever! Lets start with the basics, 1st of all, its so compact its amazing. Note : The Pic is a non-modified version of the XR-1. The XR-2 has so many add-ons.
Internal Laser Gun Sight : As you can see in the picture of the XR-1, right under the scope and in the back of it is a laser gun sight in the XR-2. The Laser Gun Sight is connected into the internal of the gun, where a REMOVABLE, unlike the LGS, solar-charge JAXBattery is, and to recharge it, let it out in the sun for 1/2 an hour. The LGS goes as far as the scope.
Scope : The scope is now equipped with night-vision, which also uses the JAXBattery. It goes farther than normal snipers in the XR-2! (I couldnt come up with an exact) The scope has also been lowered, as we got complaints it was too high.
Firing Modes : The XR-2 has 3 firing modes. Single-shot. 3x Burst Fire. And Automatic. Automatic is the favored.
Stats :
Type : Assault Rifle
Manufacterer : JaxusismCorp
Cartridge - 5.75 flechette rounds
Length - look pic
Weight - extremely light
Barrel - look pic
Magazine - 42 rounds
Rate of Fire - 1075rds/min
Muzzle Velocity - 1000m/sec
Effective Range - About 1500 yards
Comes with an Attachable 40mm M203 grenade launcher for +$200
Cost : $2,000 + 200 for Attachable Grenade Launcher
Still the light gun you love, still coming with the attachable GL. Coming with LGS. Better scope. 3 firing modes. This is a MUST BUY.
AN-94 Abakan Assault Rifle
http://weapons.0golf.com/firearms/abakan.jpg
Manufacturor: JaxusismCorp
Caliber (mm): 5,45 x 39
Principle: combined-free moving of shooting mechanism + gas engine
Range (m): 1000/650
Length (mm): 943/728
Weight (kg): 3,85
Barrel: chromade, 4 right grooves x195mm
Barrel length (mm): 405
Cycl. rate of fire (rds/m): 1800 and 600
Cost : $1,200 USD EACH
Cost: 500$
http://free.one.picturehost.co.uk/sokol314.jpg
it features the most modern electronic sighting, fire control and tactical technology.
A sharp-shooting configuration is offered as a squad weapon.
For commando, airborne, paratroopers and special rescue units, as well as tank crews, a short
Sokol-31 assault rifle is offered.
Micro Sokol is specially configured for security forces and special missions.
The Sokol-31 assault rifle is very different from other rifles. Its body is made from alloy-like metal substitutes; it is extremely lightweight, is a dark green color, and is very well insulated, so that it does not heat up after prolonged firing.
The rifle can also be equipped with a dual-purpose sight: at the press of a button, the sight can be adjusted to a laser finder, so that the rifle can be fired from hip height, using the laser to illuminate the target.
http://www.digikitten.com/playhousev2/files/pixelmonkey/solsokol.jpg
The Sokol-31 is also designed for night fighting. Night goggles can be taken from the soldier's helmet and attached to the rifle, making the red dot system effective also at night. The entire rifle was designed to be user-friendly.
The Sokol-31 was designed to have its center of balance conveniently placed and can be adjusted in minutes for left-handed use.
All the metal parts in the rifle are specially treated to avoid rusting.
http://www.digikitten.com/playhousev2/files/pixelmonkey/sokolready.jpg
Sokol-31 uses the proven, compact Bull pup design, which was optimized to best match the ergonomics and mission requirements of the modern warrior, providing natural handling, intuitive aiming from all firing positions and improved hit accuracy. Accuracy and target acquisition is enhanced, by the use of accurate aiming, through the use of an integral reflex optical reflective sight, which projects the aiming point on the center of the sight. Sokol-31 has an attachment for additional sighting devices, such as a 3rd generation night vision sight, which can be installed with no zeroing. Sokol-31 is gas operated, using rotating bolt action. it accommodates a 30 round magazine and sustain a rate of fire of 750 - 900 rounds per minute, and have the following specifications.
http://free.one.picturehost.co.uk/sokol.jpg
Specifications:
Caliber 5.45x39 mm or 7.62x39
Overall length (mm) 720 640 480
Barrel length (mm) 460 380 250
Weight empty (gr.) 2800 2700 2400
Combat weight (gr.) with: optical sight, 30 round magazine, carrying sling 3635 3535 3235
Trigger pull weight (kg) 2.5 - 4.0
Integrated sight integral red dot + laser designator
Rifling twist 6 grooves, 1:7" RH twist
Rate of fire (RPM) 1800 and 600 rounds per minute
Operation gas operation, rotating bolt
Muzzle velocity (m/sec) 890 860 770
Optional Accessories
Tele-converter
new generation night vision (no zeroing needed)
Carrying sling
20 round magazine
30 round magazine
Cleaning kit & cleaning rod
Bipod & bipod adapter
grenade launcher adapter
Arms rails
Left hand kit (bolt)
Silencer
Various sights
Blank firing attachment & magazine
Miles adapter
Short butt pad
Short (SAR) barrel
Long (sniping) barrel
It also includes the following configurations:
Sokol-31 Assault Rifle
http://free.one.picturehost.co.uk/soksault.jpg
Sokol-31 Commando Assault Rifle
http://free.one.picturehost.co.uk/sokcommando.jpg
Micro, Sokol-31 Assault Rifle
http://free.one.picturehost.co.uk/sokomicro.jpg
an updated version of the Micro-Sokol
http://www.digikitten.com/playhousev2/files/pixelmonkey/micro2s.jpg
Sharp Shooting, Sokol-31 Assault Rifle
http://www.digikitten.com/playhousev2/files/pixelmonkey/sokosniper.jpg
M40A1 7.62mm sniper rifle
http://www.fas.org/man/dod-101/sys/land/m40a1no2.jpg
Length: 44"
Weight: 14.5 lbs
Max effective range: 1000 yards
Magazine capacity: 5 rounds
Cost: $2,700
AIRCRAFT
F-15E Strike Eagle
http://s2.invisionfree.com/Outcasts/index.php?act=Attach&type=post&id=1276
Primary function: Air-to-ground attack aircraft
Power plant: Two Pratt & Whitney F100-PW-220 or 229 turbofan engines with afterburners
Thrust: 25,000 - 29,000 pounds each engine
Wingspan: 42.8 feet (13 meters)
Length: 63.8 feet (19.44 meters)
Height: 18.5 feet (5.6 meters)
Speed: Mach 2.5 plus
Maximum takeoff weight: 81,000 pounds (36,450 kilograms)
Service ceiling: 50,000 feet (15,000 meters)
Combat ceiling: 35,000 feet (10,500 meters)
Range: 2,400 miles (3,840 kilometers) ferry range with conformal fuel tanks and three external fuel tanks
Armament: One 20mm multibarrel gun mounted internally with 500 rounds of ammunition. Four AIM-7F/M Sparrow missiles and four AIM-9L/M Sidewinder missiles, or eight AIM-120 AMRAAM missiles. Any air-to-surface weapon in the Air Force inventory (nuclear and conventional)
Crew: Pilot and weapon systems officer
Unit cost: $20 Million
B-2 Spirit Stealth Bomber
http://s3.invisionfree.com/Jaxusism/index.php?act=Attach&type=post&id=3973
Primary function: Multi-role heavy bomber
Power Plant: Four General Electric F-118-GE-100 engines
Thrust: 17,300 pounds each engine
Length: 69 feet (20.9 meters)
Height: 17 feet (5.1 meters
Wingspan: 172 feet (52.12 meters
Speed: High subsonic
Ceiling: 50,000 feet (15,240 meters)
Takeoff Weight (Typical): 336,500 pounds (152,634 kilograms
Range: Intercontinental, unrefueled
Armament: Conventional or nuclear weapons
Payload: 40,000 pounds (18,144 kilograms)
Crew: Two pilots
Unit cost: $1 billion
B-1B LANCER
http://globalsecurity.org/wmd/systems/images/b1_200112122a-s.jpg
http://globalsecurity.org/wmd/systems/images/b1_mk82-s.jpg
Primary Function: Long-range, multi-role, heavy bomber
lder: Rockwell International, North American Aircraft
Operations Air Frame and Integration: Offensive avionics, Boeing Military Airplane; defensive avionics, AIL Division
Power Plant: Four General Electric F-101-GE-102 turbofan engine with afterburner
Thrust: 30,000-plus pounds (13,500-plus kilograms) with afterburner, per engine
Length: 146 feet (44.5 meters)
Wingspan: 137 feet (41.8 meters) extended forward,
79 feet (24.1 meters) swept aft
Height: 34 feet (10.4 meters)
Weight: Empty, approximately 190,000 pounds (86,183 kilograms)
Maximum Takeoff Weight: 477,000 pounds (214,650 kilograms)
Speed: 600+ mph (Mach .92) @ 500 feet
825 mph (Mach 1.25) @ 50,000 feet
Rotate and Takeoff Speeds: 210 Gross - 119 Rotate kts / 134 kts Takeoff
390 Gross - 168 kts Rotate / 183 kts Takeoff
Landing Speeds: 210 Gross - 145 kts
380 Gross - 195 kts
Range: 7,455 miles, unrefueled
3,444 miles with normal weapons load
Ceiling: 60,000 feet (18,000 meters)
Crew: Four (aircraft commander, pilot, offensive systems officer and defensive systems officer)
Armament: NUCLEAR
CONVENTIONAL
84 Mk 62
84 MK82
30 CBU 87
30 CBU 89
30 CBU 97
12 Mk 65
PRECISION
30 WCMD
24 JDAM
12 GBU-27
12 AGM-154 JSOW
12 TSSAM
Unit Cost: $200 million per aircraft
http://www.globalaircraft.org/photos/planephotos/tornado_5.jpg
Tornado IDS
Length: 54' 10"
Height: 19' 4"
Wingspan: Fully forward: 45' 2", Swept: 27' 11"
Empty Weight: 30,620 lbs
Max Takeoff Weight: 61,620 lbs
Speed: Mach 2.2
Armament: Two Mauser 27mm cannons. 19,940 lbs of assorted air to air missiles, bombs, anti-radar and anti-ship missiles. Capable of carrying the B61 nuclear bomb.
Crew: 2
Cost: $26 million. 10% discount to regional allies.
Variable geometry, multirole aircraft designed more for ground strikes than air to air, though capable of handling both.
JF stands for Joint-Fighter
Upon customer request, the JF-20 can be fitted with Western weapons such as the Vulcan cannon, AIM-120 AMRAAM, AGM-65 Maverick, etc.
The aircraft has been developed in a 50-50 partnership with Dark terror's defence ministry, the BDIA, to meet a Bisonic frontal multi-role-fighter requirement, with a naval version (JF-20K) developed to meet the needs of a new plane for the Forcien and Bisonic Navies capable of performing both attack and air superiority missions. The aircraft has easily demonstrated manoeuvres yet to be emulated by any western aircraft.
Switchblade Wing Design
The wings are attached to its fuselage (body) at a pivot point toward the back of the plane. When the wings are fully extended, the plane can fly slowly to drop bombs precisely on their targets or land on short runways. When the wings are swept farther forward, the aircraft takes advantage of the maneuverability that forward-swept wings offer, and becomes an agile fighter. When the wings are swept fully forward, the trailing edge of the wing becomes the leading edge, and the aircraft turns into a delta shape perfect for dashing away at speeds up to Mach 3.
Armament
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The JF-20 can carry up to 16 air-to-air missiles and up to 10000kg of ordnance. The fourteen external hardpoints can carry air-to-air missiles, air-to-surface missiles, bombs, rockets and an ECM (electronic countermeasures) pod. The aircraft is fitted with one Gsh-301 30mm gun with a maximum rate of fire of 1,500 rounds per minute.
The aircraft can be equipped with Vympel R-73E short-range air-to-air missiles with infrared terminal homing and RVV-AE long-range air-to-air missiles with active radar guidance. R-73E (NATO codename AA-11 Archer) is an all-aspect, close-combat missile capable of engaging targets in tail-chase or head-on mode at altitudes between 0.02 and 20km, and target g-load to 12g. The Vympel RVV-AE (AA-12 Adder) air-to-air missile, also known as the RR-77, can intercept targets at speeds up to 3,600kph and altitudes from 0.02 to 25km.
The Su-37 can be fitted with air-to-surface missiles such as the Kh-25 (AS-12 Kegler) short-range missile and Kh-29 (AS-14 Kedge) with a 317kg penetrating warhead, as well as air-launched versions of missiles such as the P-800 Yakhont (SS-N-26), Uran (SS-N-25 Switchblade), and Klub (SS-N-27), among others.
Sensors
Zhuk Multipurpose Radar
Range 175 miles. Can identify 60 targets and simultaneous track 30 target flying below
200ft while flying at 20,000ft.
E.S.M.: Radar detector, enables vehicle to detect other radars passively
Multi-target:
Can lock on and fire at up to 4 targets simultaneously with AA-13 missiles
V. A. S.: Amplify camera that allows targeting on fighter sized objects out to 30 miles
Targeting Laser/ Verifying Laser:
Used to target with laser guided weapons and to fly without using radar low to the ground
at night
the weapons management system, electronic warfare system and the Zhuk
radar work as one, giving the pilot unprecedented situation awareness.
Zhuk successfully detects air targets, manufactured with the use of "stealth" technology
The Zhuk radar is designed for air-superiority and strike operations and features a low observable, active aperture, electronically-scanned array with multi-target, all-weather capability.
The radar is key to the JF-20's integrated avionics and sensor capabilities. It will provide pilots with detailed information about multiple threats before the adversary's radar ever detects the JF-20. This is also called BVR, or Beyond Visual Range capability.
There are also systems for terrain-following and terrain-avoidance, mapping and multichannel employment of guided weapons
There is also a rear-looking NIIP NO-12 radar and optronic fire-control and surveillance system
Engines:
http://www.digikitten.com/playhousev2/files/pixelmonkey/zaengine.jpg
it uses Mach-3 G-50FU Pulse detonation engines for propulsion
the G-50FU pulse detonation engines are similar in size to modern turbojets (a bit smaller) but are more efficient because detonations create higher pressures and travel faster than turbojet combustion. This means more power, higher efficiency.
The 3-dimensional nozzle vectors thrust 20 degrees up down left and right for improved aircraft agility. This vectoring increases the roll rate of the aircraft by 50 percent and has features that contribute to the aircraft stealth requirements.
Heat-resistant components give the nozzles the durability needed to vector thrust, even in afterburner conditions.
With precision digital controls, the nozzles work like another aircraft flight control surface. Thrust vectoring is an integrated part of the Za-34's flight control system, which allows for seamless integration of all components working in response to pilot commands.
the G-50FU engines also feature:
Integrally bladed rotors: In most stages, disks and blades are made from a single piece of metal for better performance and less air leakage.
Long chord, shroud less fan blades: Wider, stronger fan blades eliminate the need for the shroud, a ring of metal around most jet engine fans. Both the wider blades and shroud less design contribute to engine efficiency.
Low-aspect, high-stage-load compressor blades: Once again, wider blades offer greater strength and efficiency.
Alloy C high-strength burn-resistant titanium compressor stators: innovative titanium alloy increases stator durability, allowing the engine to run hotter and faster for greater thrust and efficiency.
Alloy C in augmentor and nozzle: The same heat-resistant titanium alloy protects aft components, permitting greater thrust and durability.
Floatwall combustor: Thermally isolated panels of oxidation-resistant high cobalt material make the combustion chamber more durable, which helps reduce scheduled maintenance.
Fifth-generation full-authority digital electronic engine control (FADEC): Dual-redundant digital engine controls - two units per engine, two computers per unit - ensure unmatched reliability in engine control systems. The same experience that introduced full-authority digital control to fighter engines works with the aircraft system to make engine and aircraft function as a single flight unit.
No visible smoke: Reduces the possibility of an enemy visually detecting the JF-20.
Improved Supportability: All components, harnesses, and plumbing are located on the bottom of the engine for easy access, all line replaceable units (LRUs) are located one deep (units are not located on top of one another), and each LRU can be removed with just one of the six standard tools required for engine maintenance.
the JF-20 is a joint development between Dark terror and geforce4 of a new generation multi-role fighter.
The aircraft is being developed in a 50-50 partnership with Dark terror's defence ministry, to meet bisonic and forican naval multi-role-fighter requirements.
Cockpit:
http://www.digikitten.com/playhousev2/files/pixelmonkey/zacockpit.gif
The JF-20 features a side-stick controller in addition to two throttles that are the aircraft's primary flight controls. Located on the right console, the GEC-built stick also serves as a swing-out, adjustable arm rest. The stick is force sensitive and has a throw of only about one-quarter of an inch. The throttles are located on the left console.
During air combat, both the stick and the throttles are high-use controls . To support pilot functional requirements, the grips include buttons and switches (that are both shape and texture coded) to control more than 60 different time-critical functions. The buttons are used to control the offensive (weapons targeting and release) and defensive systems, (although some, like chaff and flares, can operate both automatically and manually) as well as display management.
The Heads Up Display or (HUD) server as the primary flight instrument for the pilot. It will have a viewable area of 30 degrees horizontally and 25 degrees vertically. Developed by the Air Force Instrument Flight Center, the GEC HUD will use standard symbology and be 4.5 inches in height. Unlike the HDD's, the GEC HUD will not be in color. However, the symbology will be exactly the same as the Head Down Displays. As a shock absorber from bird strikes, the windshield will be protected by a rubber buffer strip placed on the HUD combiner glass. During initial bird strike tests, the HUD would routinely shatter. Precautions were taken at all costs to avoid this from happening. The buffer strip would shield the polycarbonate glass by allowing it to flex during a strike. Design is underway for a collapsible HUD that would fall but not break. In addition, the JF-20 design also features a sort of laminate that eliminate glass from shattering in the cockpit.
The Integrated Control Panel (ICP) will be the main location where the pilot can manually input data for communications, autopilot and navigation. The ICP will be located below the HUD, underneath the glare shield and in the center top of the instrument panel. Additionally, the ICP will have "double click" features which are similar to a PC mouse in functionality. The double click feature will allow the pilot to input data more rapidly. Six Liquid crystal color displays will be housed in the cockpit. The LCD's will be fully readable in direct sunlight. Notable improvements of LCD's when compared to the older generation displays of CRT's are a lower weight, less size and a lower power consumption. The LCD's are inherently more reliable because of the lower power consumption. Two Up Front Display's (UFD)'s are located to the left and right of the ICP. They measure 3x4 inches. The primary function of the UFD's are to provide the pilot with cautionary information/warning/advisory, data communications/navigation/identification (CNI)data and act as the serve as the Stand-by Flight instrumentation Group and Fuel Quantity Indicator. A maximum of 12 messages can appear on the UFD's at any given time, and remaining faults can be indexed as sub pages.
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http://www.mach3graphics.com/misc%20graphics/jpg/SU-34%20attack.jpg
Prices:
JF-20: $50 mil
JF-20K Naval Variant: $51 mil
JF stands for Joint-Fighter
Upon customer request, the JF-20 can be fitted with Western weapons such as the Vulcan cannon, AIM-120 AMRAAM, etc.
The aircraft has been developed in a 80-20 partnership with Dark terror's defence ministry.
cost: 45 million
JF-2000 Naval VSTOL fighter and attack aircraft
http://www.aeronautics.ru/img/img006/shafagh_iran_001.jpg
G-45FU VSTOL low-observable propulsion Engine:
http://www.digikitten.com/playhousev2/files/pixelmonkey/engtest.jpg
the G-45FU advanced propulsion system utilize cutting edge technology to provide the JF-2000 with higher performance than conventional fighter aircraft. The engine consists of a 3-stage fan, a 6-stage compressor, an annual combustor, a single stage high-pressure turbine, and a 2 stage low-pressure turbine.
The STOVL propulsion system is composed G-45FU engine and the lift fan system, 3BSD and roll posts.
The front of
G-45FU engine, for example, is only a few feet inside the air intake. To avoid radar
reflections, the engine face has been hidden by special inlet guide vanes that have been
treated with RAM and shaped to cause radar beams to make multiple bounces--including
onto the air-duct walls. There, radio-frequency energy is trapped by RAM or bounced
from interior surfaces, each time being greatly attenuated. One way or another, the radar
energy becomes too weak to constitute a dangerous reflection.
there are also an intake radar blocker built as part of the face of the engine with a
bullet-like centerpiece surrounded by angled, radiating vanes. and an
infrared and radar suppression devices for jet exhausts.
the engine is coupled with a shaft-driven lift fan system for STOVL propulsion. The lift fan has been developed by Rolls-Royce Defence. Doors installed above and below the vertical fan open as the fin spins up to provide vertical lift. The main engine has a three bearing swivelling exhaust nozzle. The nozzle, which is supplemented by two roll control ducts on the inboard section of the wing, together with the vertical lift fan provide the required STOVL capability.
http://www.aeronautics.ru/img/img006/shafagh_iran_003.jpg
Sokol Array Radar (it does not move):
http://www.digikitten.com/playhousev2/files/pixelmonkey/aejfsa.jpg
Sokol uses a non-equidistant rather than the traditional linear radar field distribution, which allows a fivefold radar cost reduction over a traditionally designed phased array radar. it has a 980mm antenna diameter (37dB gain) and weigh 275kg. The radar tracks 24-30 targets, engages the most dangerous 6 to 15 of them. Its electronic beam steering will give ±70 deg spatial coverage in both axes. Power output is 8kW peak, 2 - 3kW average. It is designed for high reliability, and is frequency agile with LPI and anti ECM features. It also incorporates target identification techniques, and it is capable of interleaving between air-to-air and air-to-ground modes.
Velocity search: 300km head-on vs fighter target.
Range-while-search, lookup mode: 180-210km head-on / 100km tail-on vs fighter target.
Range-while-search, lookdown mode : 200km head-on / 80km tail-on vs fighter target.
Track-while-scan mode: 250km head-on vs fighter target.
Against a large target such as a bomber or AWACS aircraft detection range comfortably exceeds 300km.
three radar arrays placed in the nose of the aircraft (one facing forward and two facing sideways). Each wing root carried an infrared search and track system that operated through faceted windows.
Cockpit:
http://www.digikitten.com/playhousev2/files/pixelmonkey/ef2000cock.jpg[img]
The cockpit in the JF-2000 is equipped with a touch-sensitive control display, a larger multi-purpose liquid crystal color display, which shows tactical information, two monochrome displays and a new engine fuel display. The aircraft retains the mission software and a high proportion of the avionics found in the C/D models.
The cockpit also has a color digital map and the pilots are equipped with night-vision goggles.
it also features HOTTAS and a collapsible HUD that would fall but not break.
The Heads Up Display or (HUD) will server as the primary flight instrument for the pilot. It will have a viewable area of 30 degrees horizontally and 25 degrees vertically.
The Integrated Control Panel (ICP) will be the main location where the pilot can manually input data for communications, autopilot and navigation. The ICP will be located below the HUD, underneath the glare shield and in the center top of the instrument panel. Additionally, the ICP will have "double click" features which are similar to a PC mouse in functionality. The double click feature will allow the pilot to input data more rapidly. 5 Liquid crystal color displays will be housed in the cockpit. The LCD's will be fully readable in direct sunlight.
SPECIFICATIONS
Payload: 9000 KG
Length 18.4 m
Height 4.6 m
Wing span 13.6 m
Maximum speed: mach 2.1
supercruise speed: mach 1.9
Internal AA cannon: 30mm GSh-30 twin-barrel aircraft cannon
maximum operational g-loading is 9g+.
[img]http://www.islamicdigest.net/albums/albun53/Shafaq.jpg
Weaponry
The design of the JF-2000 allows a rather large weapons bay capable of holding no less than 8 air-to-air missiles (AAM?s). The JF-2000's Maximum combat load is 9,000 kg , it can also carry 4 Kh-35 (SS-N-25 Switchblade) anti-ship missiles.
When backing up ground forces, the aircraft survivability is ensured by armour protection of the critical aircraft units (which is quite a problem for the aircraft type in question) as well as by the fact, that, provided low altitudes (less then 300m) and high speeds (more then 850 km/h), such an air target is rather hard to be engaged by enemy's ground AD forces
DesignThe JF-2000 is designed to have a reduced IR and Radar signature. This gives the aircraft the stealth capabilities. The JF-2000 is also designed, to be very light ,manoeuverable and with short take off and landing capabilities. The JF-2000 has a blended fuselage and a thick wing center-section. The aerodynamic configuration of the JF-2000 is considered to be very unusual and is equipped with powerful thrust vectoring system thus providing the aircraft with unimaginable agility. The landing gear of the JF-2000 is specially designed so as to allow landing approaches at high angle of attacks.
Supermaneuverability
The swivel wing panels with leading-edge flaps allows operation in the normal flow mode within the required fuselage orientation range. This provides a higher level of controllability in the supermaneuverability modes, elimination of an involuntary spin and entering the supermaneuverability mode at higher speeds. The wing panels at negative local angles temporally reduce the maximum wing load capacity and existing loads almost two-fold. Combined with an increased controllability, this gives the aircraft a possibility to maneuver not exceeding the permissible loads. The aircraft has a full-authority digital automatic control system with a thrust controlled engine nozzle included in the longitudinal and flight control systems. The above aerodynamic characteristics will ensure the aircraft's superiority in a short-time close combat, other things being equal.
Za-41 "FireFly" ASF
cost:40 million
http://www.digikitten.com/playhousev2/files/pixelmonkey/asf41.jpg
The Advanced Strike Fighter (ASF) is a multi-role stealthy strike fighter optimized for the air-to-ground role, designed to affordably meet the needs of the Air Force, Navy, and Marine Corps, with improved survivability, precision engagement capability, the mobility necessary for future joint operations and the reduced life cycle costs.
A notable design feature of this aircraft is the enhanced survivability. The cockpit is armor protected and pushrods are used in preference to cables for the flying control surfaces. The load bearing members are strengthened. The engines are widely separated and a 10 mm thick firewall is installed between them. The explosive resistant fuel tanks are filled with reticulated foam.
The aircraft has an all-welded 30 mm titanium alloy cockpit with transparent windscreen armor block to protect the pilot and is equipped with a single K-36L Zvezda ejection seat.
Cooling air is introduced at the end of the tailcone to reduce the temperature of the exhaust gasses and minimize the infrared signature of the aircraft.
The aircraft has a carrier-suitable tailhook. Its landing gear has a longer stroke and higher load capacity.
Other Special Features:
Survivability: radio frequency/infrared signature reduction and on-board countermeasures to survive in the future battlefield.
Lethality: integration of on- and off-board sensors to enhance delivery of current and future precision weapons
Supportability: reduced logistics footprint and increased sortie generation rate to provide more combat power earlier in theater
Affordability: focus on reducing cost of developing, procuring and owning ASF to provide adequate force structure
Heads Up Display
Hands-On Throttle and Stick (HOTAS)
Internal-Weapon Bays
Super-Cruise ability
"FireFly"Advanced Towed Decoys: These are mounted in two dispensers in the fighter's tail with two decoys in the dispenser on either wing. These drones are dragged about 328 feet (100 meters) behind the aircraft on a thin cable. Each is a specially designed radar lure that creates a radar image to mimic the aircraft. The decoy has a special jammer that is designed to decoy missiles that have been programmed to home on jamming signals. If decoys are not destroyed, they can be recovered and repaired.
ASF?s integrated avionics and stealth are intended to allow it to penetrate surface-to-air missile defenses to destroy targets, when enabled by air dominance. The ASF is designed to complement a force structure that includes other stealthy and non-stealthy fighters, bombers, and reconnaissance / surveillance assets.
The cockpit interior lighting is fully Night Vision Goggle (NVG) compatible, as is the exterior lighting. The cockpit panels feature extended life, self-balancing, electro luminescent (EL) edge-lit panels with an integral life-limiting circuit that runs the lights at the correct power setting throughout their life. It starts at one-half power and gradually increases the power output to insure consistent panel light intensity over time. As a result, the cockpit always presents a well-balanced lighting system to the pilot (there is not a mottled look in the cockpit). The panels produce low amounts of heat and power and are very reliable.
The aircraft also has integral position and anti-collision lights (including strobes) on the wings. The low voltage electro luminescent formation lights are located at critical positions for night flight operations on the aircraft (on the forward fuselage (both sides) under the chine, on the tip of the upper left and right wings, and on the outside of both vertical stabilizers. There are similar air refueling lights on the butterfly doors that cover the air refueling receptacle.
This aircraft packs state of the art sensors and communications equipment. Among it's many features is an enhanced radar system that can track up to 128 targets simultaneously out to a range of 250 miles (400 km). Any targets acquired by the radar are fed into the vehicle's targeting computers
the aircraft can fire missiles at up to 15 targets at the same time. It is also capable of Terrain Following for low altitude flight.
Stealth:
Radar Absorbing Material is covering the entire fuselage of the za-41. This material is made to absorb and kill radio waves instead of reflect
them.
the over-all shape of the aircraft has angles to it that scrambles the radar all over, everywhere but back to the radar's origin.
it also has special horizontal stabilizers located on the aft part of the aircraft. These stabilizers help evenly distribute the lift of the aircraft so that moisture Contrails are avoidable.
Specifications:
2 SKF-40E Pulse Detonation Engines with robust rotary valves [they use a two-stage ignition process to achieve detonation.]
detonation is a violent explosion and as such it produces vastly higher pressures than the simple burning process of deflagration.
Maximum Speed: Mach 4+
Supercruise speed: mach 3-3.2
ceiling: 110,000 ft
G-load: 9
range with external fuel tanks: 4,600 kilometres
Gun : one GSh-301
Ammunition 600 rounds
Firing rate 1,500 rounds per minute
Max Payload, 25,640 lb
Air-to-Air Missiles: up to 13
and large variety of Air-to-Surface Missiles including anti-ship
Bombs:laser-guided bombs and other advanced bombs.
Other: rocket pods, ECM pods
Please note:
Dealer and manufacturer (production) rights are reserved to Geforce4 only!
Thank you for your understanding.©
Ezh-444MCA Multi-Sensor Command and Control Aircraft [ AESA equiped ]
cost: 800 million credits
http://www.boeing.com/news/feature/concept/images/010426a.jpg
Ezh-444MCA is an aircraft that could support capabilities currently delivered by AWACS, Joint STARS, and the Airborne Command and Control Center all Together!, it provides the military with an aircraft capable of serving as an intelligence, surveillance and reconnaissance (ISR) platform fully interoperable with other aircraft and unmanned systems.
Specifications:
Environmental benefits include landings and takeoffs quieter than Stage 4 airplanes and the same fuel burn as today's best performers.
http://www.boeing.com/news/feature/concept/images/k61686.jpg
Maximum cruising Altitude: Mid-40,000-foot level or higher (13,000 meters+)
Coverage 360º air and maritime
Tracking capability more than 3500 targets
Crew: Two flight crew and up to 10 mission crew
Range: Between 6,000 and 9,000 nautical miles
Max Speed: mach 1.1
Endurance: 25 hours, with 800 km radius of action
Cockpit: http://www.airforce-technology.com/projects/737aewc/images/737AEWC_3.jpg
Ezh-444 Tanker Version
cost: 40 million
http://www.boeing.com/news/feature/concept/images/concept.jpg
it can itself be refueled in flight. It also have the capability to refuel Air Force, Navy, Marine and other aircraft on every mission!.
Equipped with both the proven boom-and-receptacle and the hose-and-drogue aerial refueling systems, the Ezh-444 Tanker/Transport offers maximum operational flexibility, Ezh-444 Tanker/Transport is really four aircraft in one. While maintaining its tanker capability, the aircraft's uninterrupted cabin floor can be configured for: Passenger; Freighter; Convertible (passenger or freighter); and Combi (passenger and freighter).
The installation of wingtip refuelling pods involves a major modification and refit to the entire aircraft, including modifications to the wing and fuselage fuel tanks, additional fuel control systems and the installation of indicators and circuit breakers on the flight deck.
Inside the refuelling pods, a collapsible funnel-shaped drogue is attached to a hose, which is reeled out to trail behind the wing of the aircraft. The hose is fitted with a constant tension spring to give stability to the hose while it is extended.
Orel AEW&CS aircraft
cost: 270 million
http://www.spyflight.co.uk/images/JPGS/Boeing%20707/707%20Condor%20port.jpg
http://www.spyflight.co.uk/images//JPGS/Boeing%20707/707%20Condor%20starboard.jpg
http://www.spyflight.co.uk/images/JPGS/Boeing%20707/phalcon.jpg
The world's most advanced AEWC&C system, the OREL, was developed and produced by Geforce using Active Phased Array Electronic Scanning Technology rather than a mechanically rotating antenna (rotodome) used by current AWACS systems, giving OREL greater operational flexibility and performance by several orders of magnitude. The Orel AEW&C aircraft is based on four sensors: phased-array radar, phased-array IFF, ESM/ELINT and CSM/COMINT. A unique fusion technology continuously cross-relates the data gathered by all sensors. When one of the sensors reports a detection, the system automatically initiates an active search of the complementary sensors.
The AWE&C phased array radar replaces the conventional rotodome radar. It is mounted either on the aircraft fuselage or on top of the aircraft inside a stationary dome, providing full 360° coverage. This electronically steered beam radar delivers a tremendous advantage over mechanical rotating antenna, as it supports the tracking a high maneuvering targets. The radar can detect even low flying objects from distances of hundreds of kilometers, day and night, under all weather conditions. Verification beams sent at specific, individual, newly detected targets eliminate false alarms. Moreover, track initiation is achieved in 2 to 4 seconds as compared to 20 to 40 seconds with a rotodome radar
The IFF system employs solid state phased array technology to perform interrogation, decoding, target detection and tracking. A monopulse technique is used to implement azimuth measurement. The IFF data is automatically correlated with the phased array radar.
The ESM/ELINT system receives, analyzes and locates radar signals, covering 360o. It combines high sensitivity with high probability of intercept, and achieves excellent accuracy in bearing measurement. The system uses narrow-band super-heterodyne receivers and wide-band instantaneous frequency measurement (IFM) techniques to provide very high accuracy and probability of intercept of airborne and surface emitters. Very high bearing accuracy for all received signals is achieved through Differential Time of Arrival (DTOA) measurements. The system also collects and analyzes ELINT data.
The Orel's CSM/COMINT receives in UHF, VHF and HF, rapidly searching for airborne, shipborne or ground communications signals of interest. Selected radio nets can be monitored for signal activity. A DF capability locates targets. Detected signals can be assigned to monitoring receivers instantaneously. The system makes extensive use of computers to reduce the load on operators.
specifications:
Wing Span: 44.60 m
Wing Area: 283.40 m²
Length: 44.40 m
Height: 12.90 m
Engine 4 x P&W JT3D-3B
Maximum speed: 973 Km/h
Range 6,920 Km
Primary Radar
Type electronically scanned array, all weather
Frequency L-band
Coverage 360º air and maritime
Range more than 300nm
IFF range 400nm
Tracking capability more than 2700 targets
Multi role mission consoles 5
naval AWACS Orel-45
cost: 120 million
http://homepage.tinet.ie/%7Esteven/images/hawkeyefr8.jpg
The AN/AGPS-170 radar is capable of tracking more than 2,000 targets and controlling the interception of 70 hostile targets. One radar sweep covers 6 million cubic miles. The radar's total radiation aperture control antenna reduces sidelobes and is robust against electronic countermeasures. It is capable of detecting aircraft at ranges greater than 550km.
The mission computer is equipped with an enhanced high-speed parallel processor. advanced display system and computer peripherals provide the operators with multicolour displays, map overlays, zoom facilities and auxiliary data displays.
Secondary roles of the Orel-45 include strike command and control, surveillance as well as guidance of search and rescue missions
Specification:
Cruise speed, km/h 750
Range 500 km with 6 hr 30 min on station
Endurance 6 hr 15 min
Detection range of aircraft greater than 550 km
HELICOPTERS
AH-64A/D Apache Attack Helicopter
http://www.military.com/Data/EQG/ah64_large.jpg
http://www.fas.org/man/dod-101/sys/ac/ah-64d-image25.jpg
This is the battle tested Apache available in standard and Longbow variants. Both have one M230 30mm gun and can carry 70mm (2.75 inch) Hydra-70 folding-fin rockets, up to 16 AGM-114 Hellfire anti-tank missiles, AGM-122 Sidearm anti-radar missiles, AIM-9 Sidewinder or FIM-92 Stinger air-to-air missiles, and have nightvision and low-light vision systems standard. The Longbow comes complete with advanced targeting systems, a mushroom shaped powerful radar, and the ability to carry Hellfire MMW air to surface/air to air missiles.(Longbow shown in image)
Max speed is 163 knots
Crew is 2
Each AH-64A Apache costs $15.4 million
Each AH-64D Longbow costs $17.2 million
AH-64A Apache Attack Helicopter
http://s3.invisionfree.com/Jaxusism/index.php?act=Attach&type=post&id=3977
Propulsion Two T700-GE-701Cs
Crew Two
Length 58.17 ft (17.73 m) 58.17 ft (17.73 m)
Height 15.24 ft (4.64 m) 13.30 ft (4.05 m)
Wing Span 17.15 ft (5.227 m) 17.15 ft (5.227 m)
Primary Mission Gross Weight 15,075 lb (6838 kg)11,800 pounds Empty 16,027 lb (7270 kg) Lot1
Weight Hover In-Ground Effect (MRP) 15,895 ft (4845 m)
Hover Out-of-Ground Effect (MRP) 12,685 ft (3866 m)
Maximum Level Flight Speed 150 kt (279 kph)
Range 400 km - internal fuel 1,900 km - internal and external fuel
Armament: Primary MissionStarboard WingM230 GunPort WingRate of ClimbDurationCombat (Anti-armor)
4 Hellfire320 rds 30mm
4 Hellfire1450 fpm1.8 hours
Multi-role (Covering force)
4 Hellfire 19 FFAR *1200 rds 30mm
4 Hellfire 19 FFAR *860 fpm2.5 hours
Close-support (Anti-armor)
8 Hellfire1200 rds 30mm
8 Hellfire990 fpm2.5 hours
Ground-support (Airmobile escort)38 FFAR *1200 rds 30mm38 FFAR *780 fpm2.5 hours
M230 33mm Gun
70mm (2.75 inch) Hydra-70 Folding-Fin Aerial Rockets
AGM-114 Hellfire anti-tank missiles
AGM-122 Sidearm anti-radar missile
AIM-9 Sidewinder Air-to-Air missiles
Unit Cost: $23 Million
MISSILES
AIM-9 SIDEWINDER
http://www.af.mil/media/factsheet/aim_9.jpg
FEATURES
The AIM-9 has a cylindrical body with a roll-stabilizing rear wing/rolleron assembly. Also, it has detachable, double-delta control surfaces behind the nose that improve the missile's maneuverability. Both rollerons and control surfaces are in a cross-like arrangement.
The missile's main components are an infrared homing guidance section, an active optical target detector, a high-explosive warhead and a rocket motor.
The infrared guidance head enables the missile to home in on target aircraft engine exhaust. An infrared unit costs less than other types of guidance systems, and can be used in day/night and electronic countermeasures conditions. The infrared seeker also permits the pilot to launch the missile, then leave the area or take evasive action while the missile guides itself to the target.
General Characteristics
Primary Function: Air-to-air missile
Power Plant: Hercules and Bermite Mk 36 Mod 11
Length: 9 feet, 5 inches (2.87 meters)
Diameter: 5 inches (0.13 meters)
Finspan: 2 feet, 3/4 inches (0.63 meters)
Warhead: Annular blast fragmentation warhead
Launch Weight: 190 pounds (85.5 kilograms)
Guidance System: Solid-state, infrared homing system
Unit Cost: Approximately $84,000
AGM-88 HARM
http://www.af.mil/media/factsheet/agm88.jpg
FEATURES
The AGM-88 can detect, attack and destroy a target with minimum aircrew input. The proportional guidance system that homes in on enemy radar emissions has a fixed antenna and seeker head in the missile nose. A smokeless, solid-propellant, dual-thrust rocket motor propels the missile. The F-16C has the capability to employ the AGM-88, and is the only aircraft in the current inventory to use the AGM-88.
General Characteristics
Primary Function: Air-to-surface anti-radiation missile
Thrust: Dual thrust
Length: 13 feet, 8 inches (4.14 meters)
Launch Weight: 800 pounds (360 kilograms)
Diameter: 10 inches (25.40 centimeters)
Wingspan: 3 feet, 8 inches (101.60 centimeters)
Range: 30 plus miles (48 plus kilometers)
Speed: Supersonic
Aircraft: Used aboard the F-16C
Guidance System: Proportional
Warheads: High explosive
Unit Cost: $200,000
JAXMi2 Missiles : VERY explosive missiles. One missile capable of destroying an entire CITY! How did they come to be? An unidentified liquid was found and tested and found to be extremely explosive. More information on JAXMi2 Here (http://www.nationstates.net/forum/viewtopic.php?t=89886)!
Cost : $1 billion USD EACH
AIM-120 AMRAAM
http://www.af.mil/media/factsheet/aim120.jpg
FEATURES
The AMRAAM program improves the aerial combat capabilities of U.S. and allied aircraft to meet current and future threat of enemy air-to-air weapons. AMRAAM is compatible with the Air Force F-15, F-16 and developmental F-22; Navy F-14 D/D (R) and F/A-18 C/D; German F-4 and the British Sea Harrier aircraft.
AMRAAM is a follow-on to the AIM-7 Sparrow missile series. The missile is faster, smaller and lighter, and has improved capabilities against low-altitude targets. It incorporates active radar with an inertial reference unit and micro-computer system, which makes the missile less dependent upon the fire-control system of the aircraft. Once the missile closes on a target, its active radar guides it to intercept. This enables the pilot to aim and fire several missiles simultaneously at multiple targets. The pilot may then perform evasive maneuvers while the missiles guide themselves to their targets.
General Characteristics
Primary Function: Air-to-air tactical missile
Length: 143.9 inches (366 centimeters)
Launch Weight: 335 pounds (150.75 kilograms)
Diameter: 7 inches (17.78 centimeters)
Wingspan: 20.7 inches (52.58 centimeters)
Range: 20+ miles (17.38+ nautical miles)
Speed: Supersonic
Guidance System: Active radar terminal/inertial midcourse
Warhead: Blast fragmentation
Unit Cost: $386,000
AIM-7 SPARROW
http://www.af.mil/media/photodb/web/web_030819-F-8888Z-003.jpg
FEATURES
The missile has four major sections: guidance section, warhead, control and rocket motor. It has a cylindrical body with four wings at mid-body and four tail fins. Although external dimensions of the Sparrow remained relatively unchanged from model to model, the internal components of newer missiles represent major improvements with vastly increased capabilities.
General Characteristics
Primary Function: Air-to-air guided missile
Length: 12 feet (3.64 meters)
Diameter: 8 inches (0.20 meters)
Wingspan: 3 feet, 4 inches (1 meter)
Warhead: Annular blast fragmentation warhead
Launch Weight: Approximately 500 pounds (225 kilograms)
Guidance System: Raytheon semiactive on either continuous wave or pulsed Doppler radar energy
Unit Cost: $125,000
JOINT DIRECT ATTACK MUNITIONS GBU 31/32
http://www.af.mil/media/factsheet/jdam.jpg
FEATURES
JDAM is a guided air-to-surface weapon that uses either the 2,000-pound BLU-109/MK 84 or the 1,000-pound BLU-110/MK 83 warheads as the payload. JDAM enables employment of accurate air-to-surface weapons against high priority fixed and relocatable targets from fighter and bomber aircraft. Guidance is facilitated through a tail control system and a GPS-aided INS. The navigation system is initialized by transfer alignment from the aircraft that provides position and velocity vectors from the aircraft systems.
Once released from the aircraft, the JDAM autonomously navigates to the designated target coordinates. Target coordinates can be loaded into the aircraft before takeoff, manually altered by the aircrew before weapon release, and automatically entered through target designation with onboard aircraft sensors. In its most accurate mode, the JDAM system will provide a weapon circular error probable of 13 meters or less during free flight when GPS data is available. If GPS data is denied, the JDAM will achieve a 30-meter CEP or less for free flight times up to 100 seconds with a GPS quality handoff from the aircraft.
JDAM can be launched from very low to very high altitudes in a dive, toss and loft or in straight and level flight with an on-axis or off-axis delivery. JDAM enables multiple weapons to be directed against single or multiple targets on a single pass.
JDAM is currently compatible with B-1B, B-2A, B-52H, F-15E, F-14A/B/D, F/A-18E/F, F-16C/D and F/A-18C/D aircraft. Follow-on integration efforts are currently underway or planned to evaluate compatibility with the A-10, F/A-22, F-117, AV-8B, S-3, and the Joint Strike Fighter.
General Characteristics
Primary Function: Guided air-to-surface weapon
Length: (JDAM and warhead) GBU-31 (v) 1/B: 152.7 inches (387.9 centimeters); GBU-31 (v) 3/B: 148.6 inches (377.4 centimeters); GBU-32 (v) 1/B: 119.5 inches (303.5 centimeters)
Launch Weight: (JDAM and warhead) GBU-31 (v) 1/B: 2,036 pounds (925.4 kilograms); GBU-31 (v) 3/B: 2,115 pounds (961.4 kilograms); GBU-32 (v) 1/B: 1,013 pounds (460.5 kilograms)
Wingspan: GBU-31: 25 inches (63.5 centimeters); GBU-32: 19.6 ins. (49.8 centimeters)
Range: Up to 15 miles
Ceiling: 45,000-plus feet (13,677 meters)
Guidance System: GPS/INS
Unit cost: Approximately $21,000 per tailkit
LG-118A PEACEKEEPER
http://www.af.mil/media/factsheet/lg118.jpg
FEATURES
The Peacekeeper is capable of delivering 10 independently targeted warheads with greater accuracy than any other ballistic missile.. It is a four-stage rocket ICBM system consisting of three major sections: the boost system, the post-boost vehicle system and the re-entry system.
The boost system consists of four rocket stages that launch the missile into space. These rocket stages are mounted atop one another and fire successively. Each of the first three stages exhausts its solid propellant materials through a single movable nozzle that guides the missile along its flight path.
Following the burnout and separation of the boost system's third rocket stage, the fourth stage post-boost vehicle system, in space, maneuvers to deploy the re-entry vehicles in sequence.
The post-boost vehicle system is the Peacekeeper Stage IV that has a guidance and control system and re-entry system. The post-boost vehicle rides atop the boost system, weighs about 2,500 pounds (1,333 kilograms) and is 3.5 feet (1.07 meters) long.
The top section of the Peacekeeper is the re-entry system. It consists of the deployment module, up to 10 cone-shaped re-entry vehicles and a protective shroud. The shroud protects the re-entry vehicles during ascent. It is topped with a nose cap, containing a rocket motor to separate it from the deployment module.
The deployment module provides structural support for the re-entry vehicles and carries the electronics needed to activate and deploy them. The vehicles are covered with material to protect them during re-entry through the atmosphere to their targets and are mechanically attached to the deployment module. The attachments are unlatched by gas pressure from an explosive cartridge broken by small, exploding bolts, which free the re-entry vehicles, allowing them to separate from the deployment module with little disturbance. Each deployed re-entry vehicle follows a ballistic path to its target.
General Characteristics
Primary Function: Strategic deterrence
Warheads: 10
Load: Avco MK21 re-entry vehicles
Guidance System: Inertial; integration by Boeing North American, IMU by Northrop and Boeing North American
Thrust: First stage, 500,000 pounds
Length: 71 feet (21.8 meters)
Weight: 195,000 pounds (87,750 kilograms) including re-entry vehicles
Diameter: 7 feet, 8 inches (2.3 meters)
Range: Greater than 6,000 miles (5,217 nautical miles)
Speed: Approximately 15,000 miles per hour at burnout (Mach 20 at sea level)
Unit Cost: $70 million
LGM-30 MINUTEMAN III
http://www.af.mil/media/photodb/web/web_030813-F-8888U-005.jpg
FEATURES
The Minuteman is a strategic weapon system using a ballistic missile of intercontinental range. Missiles are dispersed in hardened silos to protect against attack and connected to an underground launch control center through a system of hardened cables. Launch crews, consisting of two officers, perform around-the-clock alert in the launch control center.
A variety of communication systems provide the president and secretary of defense with highly reliable, virtually instantaneous direct contact with each launch crew. Should command capability be lost between the launch control center and remote missile launch facilities, specially configured E-6B airborne launch control center aircraft automatically assume command and control of the isolated missile or missiles. Fully qualified airborne missile combat crews aboard airborne launch control center aircraft would execute the president's orders.
An extensive life extension program is under way to keep the missiles safe, secure and reliable well into the 21st century. These major programs include: replacement of the aging guidance system, remanufacture of the solid-propellant rocket motors, replacement of standby power systems, repair of launch facilities, and installation of updated, survivable communications equipment, and new command and control consoles to enhance immediate communications.
General Characteristics
Primary Function: Intercontinental ballistic missile
Length: 59.9 feet (18 meters)
Weight: 79,432 pounds (32,158 kilograms)
Diameter: 5.5 feet (1.67 meters)
Range: 6,000-plus miles (5,218 nautical miles)
Speed: Approximately 15,000 mph (Mach 23 or 24,000 kph) at burnout
Ceiling: 700 miles (1,120 kilometers)
Thrust: First stage, 202,600 pounds
Load: Re-entry vehicle: Lockheed Martin Missiles and Space MK 12 or MK 12A
Guidance systems: Inertial system: Boeing North American; ground electronic/security system: Sylvania Electronics Systems and Boeing Co.
Unit cost: $7 million
RIM-7 SEA SPARROW
http://globalsecurity.org/military/systems/munitions/images/seasparrow-atsea39-s.jpg
POWEer Plant Hercules MK-58 solid-propellant rocket motor
Thrust Classified
Speed More than 2,660 mph (4,256 kph)
Range More than 30 nautical miles (approximately 55 km)
[Maximum Range = 6 nm according to other sources]
Minimum Range - 1600 yards
Director Lock-on Range - 50 nautical miles
Length 12 feet (3.64 meters)
Diameter 8 inches (20.3 cm)
Wingspan 3 feet 4 inches (one meter)
Warhead Annular blast fragmentation warhead, 90 pounds (40.5 kg)
Proximity fuzed, continuous expanding rod, with a 27 ft. kill radius
fire control systems MK 91
Launch Platform (Launcher) MK 29 Mod 1.
Launch Weight Approximately 500 pounds (225 kg)
Guidance System Raytheon semi-active on continuous wave or pulsed Doppler radar energy
Date Deployed 1976
Unit Cost $165,400
BGM-109 Tomahawk
http://www.fas.org/man/dod-101/sys/smart/slcm-dvic470.jpg
Length: 18 feet 3 inches (5.56 meters); with booster: 20 feet 6 inches (6.25 meters)
Weight: 2,650 pounds (1192.5 kg); 3,200 pounds (1440 kg) with booster
Diameter: 20.4 inches (51.81 cm)
Wing Span (when deployed): 8 feet 9 inches (2.67 meters)
Range: Land attack, conventional warhead: 600 nautical miles
Speed: Approx. 550 mph
Warheads: Conventional 1000 lb high explosive warhead OR conventional munition bomblet dispenser OR 200 kiloton W-80 nuclear warhead. Comes with standard high explosive warhead.
Cost: $750,000
Launched from the sea via a torpedo tube, Vertical Launch System, or Armored Box Launcher, this highly destructive, highly accurate, and highly versatile missile has been the main land attack missile of the American navy for the last decade. It is also highly accurate, with only a handful of booster failures in its history, and a 90%+ strike success rate in both Iraq and Bosnia. Great addition to any navy.
NAVAL
SSN-21 SEA WOLF SUBMARINE
http://globalsecurity.org/military/systems/ship/images/ssn-21-dvic117-s.jpg
Builders General Dynamics Electric Boat Division
Power Plant One S6W reactor
one shaft at with 52,000 shp with pumpjet propulsor
Improved Performance Machinery Program Phase II one secondary propulsion submerged motor
Length 353 feet (107.6 meters)
Draft 35 feet (10.67 meters)
Beam 40 feet (12.2 meters)
Displacement 7,460 ton surface displacement
9,137 tons submerged displacement
Speed Official: 25+ knots (28+ miles per hour, 46.3+ kph)
Actual: 35 knots maximum submerged speed
Actual: 20 knots tactical ["silent"] speed
Operating Depth Official: "greater than 800 feet"
Actual: About 1600 feet
Jane's Fighting Ships: 2000 feet
Armament eight 660-mm torpedo tubes
50 Tomahawk cruise missiles or
50 Harpoon antiship missiles or
50 Mark 48 ADCAP torpedoes or
up to 100 mines Systems AN/BSY-2 active-passive Sonar/Fire Control w/
hemispherical bow array and wide aperture array
TB-16B or TB-23 towed array
AN/BPS-16 search and navigation radar
AN/WLQ-4(V)1 ES receiver
Central Combat System (CCS) MK2
Link 11 Tactical data link
OTCIXS Tactical data link
Crew 12 Officers; 121 Enlisted
Price : 900million
JAX Modified IOWA-CLASS Battle Ship
http://globalsecurity.org/military/systems/ship/images/missour2-s.jpg
length:888ft
beam:109ft
draft:38ft
max speed:35knots
powerplants:8boilers,4geared turbines,4shafts,212,000shaft horse power.
Armament 32 - Tomahawk ASM/LAM - 8 armored box launchers
16 - Harpoon ASM - 4 quad cell launchers
9 - Mk 7 - 16-inch / 50 caliber guns
12 - Mk 28 - 5-inch / 38 caliber guns
4 - Mk 15 - 20mm Phalanx CIWS
Combat Systems SPS-49 Air Search Radar
SPS-67 Surface Search Radar
4 Mk37 Gun Fire Control
2 Mk38 Gun Direction
1 Mk40 Gun Director
1 SPQ-9 [BB-61] SLQ-25 NIXIE
SLQ-32 EW system
Aircraft None embarked
landing area and unhangared parking area
4 SH-3 or
4 SH-60
Crew : 65officers, 1450 enlisted, 58marines.
Price : 4 billion
NOTE : Armacor has now joined up with JF in a sorta I supply him he supply my customer sorta thing!
For Sale :
GUNS
XR-1 (X-Rifle)
http://defence-data.com/dsei99/sar21.jpg
Type : Assault Rifle
Manufacterer : JaxusismCorp
Cartridge - 5.56mm
Length - look pic
Weight - light
Barrel - look pic
Magazine - 40 rounds
Rate of Fire - 950rds/min
Muzzle Velocity - 985m/sec
Effective Range - About 1000 yards
Comes with an Attachable 40mm M203 grenade launcher for +$200
Scope with Zoom capabilities for, well, a long range.
Cost : $1,400 + 200 for Attachable Grenade Launcher
Extremely light and a pretty nice size, this assault rifle, the XR-1, spreads 950 rounds a minute. Its range goes about 1000 yards. The scope has zooming capabilities for a long range. And, for 200 extra, you get the attachable 40mm M203 grenade launcher. Buy yours today!
XR-2 (X-Rifle)
NOTE : PIC IS XR-1!! NOT XR-2!!!
http://defence-data.com/dsei99/sar21.jpg
Well, here it is, the XR-2, probably the best rifle ever! Lets start with the basics, 1st of all, its so compact its amazing. Note : The Pic is a non-modified version of the XR-1. The XR-2 has so many add-ons.
Internal Laser Gun Sight : As you can see in the picture of the XR-1, right under the scope and in the back of it is a laser gun sight in the XR-2. The Laser Gun Sight is connected into the internal of the gun, where a REMOVABLE, unlike the LGS, solar-charge JAXBattery is, and to recharge it, let it out in the sun for 1/2 an hour. The LGS goes as far as the scope.
Scope : The scope is now equipped with night-vision, which also uses the JAXBattery. It goes farther than normal snipers in the XR-2! (I couldnt come up with an exact) The scope has also been lowered, as we got complaints it was too high.
Firing Modes : The XR-2 has 3 firing modes. Single-shot. 3x Burst Fire. And Automatic. Automatic is the favored.
Stats :
Type : Assault Rifle
Manufacterer : JaxusismCorp
Cartridge - 5.75 flechette rounds
Length - look pic
Weight - extremely light
Barrel - look pic
Magazine - 42 rounds
Rate of Fire - 1075rds/min
Muzzle Velocity - 1000m/sec
Effective Range - About 1500 yards
Comes with an Attachable 40mm M203 grenade launcher for +$200
Cost : $2,000 + 200 for Attachable Grenade Launcher
Still the light gun you love, still coming with the attachable GL. Coming with LGS. Better scope. 3 firing modes. This is a MUST BUY.
AN-94 Abakan Assault Rifle
http://weapons.0golf.com/firearms/abakan.jpg
Manufacturor: JaxusismCorp
Caliber (mm): 5,45 x 39
Principle: combined-free moving of shooting mechanism + gas engine
Range (m): 1000/650
Length (mm): 943/728
Weight (kg): 3,85
Barrel: chromade, 4 right grooves x195mm
Barrel length (mm): 405
Cycl. rate of fire (rds/m): 1800 and 600
Cost : $1,200 USD EACH
Cost: 500$
http://free.one.picturehost.co.uk/sokol314.jpg
it features the most modern electronic sighting, fire control and tactical technology.
A sharp-shooting configuration is offered as a squad weapon.
For commando, airborne, paratroopers and special rescue units, as well as tank crews, a short
Sokol-31 assault rifle is offered.
Micro Sokol is specially configured for security forces and special missions.
The Sokol-31 assault rifle is very different from other rifles. Its body is made from alloy-like metal substitutes; it is extremely lightweight, is a dark green color, and is very well insulated, so that it does not heat up after prolonged firing.
The rifle can also be equipped with a dual-purpose sight: at the press of a button, the sight can be adjusted to a laser finder, so that the rifle can be fired from hip height, using the laser to illuminate the target.
http://www.digikitten.com/playhousev2/files/pixelmonkey/solsokol.jpg
The Sokol-31 is also designed for night fighting. Night goggles can be taken from the soldier's helmet and attached to the rifle, making the red dot system effective also at night. The entire rifle was designed to be user-friendly.
The Sokol-31 was designed to have its center of balance conveniently placed and can be adjusted in minutes for left-handed use.
All the metal parts in the rifle are specially treated to avoid rusting.
http://www.digikitten.com/playhousev2/files/pixelmonkey/sokolready.jpg
Sokol-31 uses the proven, compact Bull pup design, which was optimized to best match the ergonomics and mission requirements of the modern warrior, providing natural handling, intuitive aiming from all firing positions and improved hit accuracy. Accuracy and target acquisition is enhanced, by the use of accurate aiming, through the use of an integral reflex optical reflective sight, which projects the aiming point on the center of the sight. Sokol-31 has an attachment for additional sighting devices, such as a 3rd generation night vision sight, which can be installed with no zeroing. Sokol-31 is gas operated, using rotating bolt action. it accommodates a 30 round magazine and sustain a rate of fire of 750 - 900 rounds per minute, and have the following specifications.
http://free.one.picturehost.co.uk/sokol.jpg
Specifications:
Caliber 5.45x39 mm or 7.62x39
Overall length (mm) 720 640 480
Barrel length (mm) 460 380 250
Weight empty (gr.) 2800 2700 2400
Combat weight (gr.) with: optical sight, 30 round magazine, carrying sling 3635 3535 3235
Trigger pull weight (kg) 2.5 - 4.0
Integrated sight integral red dot + laser designator
Rifling twist 6 grooves, 1:7" RH twist
Rate of fire (RPM) 1800 and 600 rounds per minute
Operation gas operation, rotating bolt
Muzzle velocity (m/sec) 890 860 770
Optional Accessories
Tele-converter
new generation night vision (no zeroing needed)
Carrying sling
20 round magazine
30 round magazine
Cleaning kit & cleaning rod
Bipod & bipod adapter
grenade launcher adapter
Arms rails
Left hand kit (bolt)
Silencer
Various sights
Blank firing attachment & magazine
Miles adapter
Short butt pad
Short (SAR) barrel
Long (sniping) barrel
It also includes the following configurations:
Sokol-31 Assault Rifle
http://free.one.picturehost.co.uk/soksault.jpg
Sokol-31 Commando Assault Rifle
http://free.one.picturehost.co.uk/sokcommando.jpg
Micro, Sokol-31 Assault Rifle
http://free.one.picturehost.co.uk/sokomicro.jpg
an updated version of the Micro-Sokol
http://www.digikitten.com/playhousev2/files/pixelmonkey/micro2s.jpg
Sharp Shooting, Sokol-31 Assault Rifle
http://www.digikitten.com/playhousev2/files/pixelmonkey/sokosniper.jpg
M40A1 7.62mm sniper rifle
http://www.fas.org/man/dod-101/sys/land/m40a1no2.jpg
Length: 44"
Weight: 14.5 lbs
Max effective range: 1000 yards
Magazine capacity: 5 rounds
Cost: $2,700
AIRCRAFT
F-15E Strike Eagle
http://s2.invisionfree.com/Outcasts/index.php?act=Attach&type=post&id=1276
Primary function: Air-to-ground attack aircraft
Power plant: Two Pratt & Whitney F100-PW-220 or 229 turbofan engines with afterburners
Thrust: 25,000 - 29,000 pounds each engine
Wingspan: 42.8 feet (13 meters)
Length: 63.8 feet (19.44 meters)
Height: 18.5 feet (5.6 meters)
Speed: Mach 2.5 plus
Maximum takeoff weight: 81,000 pounds (36,450 kilograms)
Service ceiling: 50,000 feet (15,000 meters)
Combat ceiling: 35,000 feet (10,500 meters)
Range: 2,400 miles (3,840 kilometers) ferry range with conformal fuel tanks and three external fuel tanks
Armament: One 20mm multibarrel gun mounted internally with 500 rounds of ammunition. Four AIM-7F/M Sparrow missiles and four AIM-9L/M Sidewinder missiles, or eight AIM-120 AMRAAM missiles. Any air-to-surface weapon in the Air Force inventory (nuclear and conventional)
Crew: Pilot and weapon systems officer
Unit cost: $20 Million
B-2 Spirit Stealth Bomber
http://s3.invisionfree.com/Jaxusism/index.php?act=Attach&type=post&id=3973
Primary function: Multi-role heavy bomber
Power Plant: Four General Electric F-118-GE-100 engines
Thrust: 17,300 pounds each engine
Length: 69 feet (20.9 meters)
Height: 17 feet (5.1 meters
Wingspan: 172 feet (52.12 meters
Speed: High subsonic
Ceiling: 50,000 feet (15,240 meters)
Takeoff Weight (Typical): 336,500 pounds (152,634 kilograms
Range: Intercontinental, unrefueled
Armament: Conventional or nuclear weapons
Payload: 40,000 pounds (18,144 kilograms)
Crew: Two pilots
Unit cost: $1 billion
B-1B LANCER
http://globalsecurity.org/wmd/systems/images/b1_200112122a-s.jpg
http://globalsecurity.org/wmd/systems/images/b1_mk82-s.jpg
Primary Function: Long-range, multi-role, heavy bomber
lder: Rockwell International, North American Aircraft
Operations Air Frame and Integration: Offensive avionics, Boeing Military Airplane; defensive avionics, AIL Division
Power Plant: Four General Electric F-101-GE-102 turbofan engine with afterburner
Thrust: 30,000-plus pounds (13,500-plus kilograms) with afterburner, per engine
Length: 146 feet (44.5 meters)
Wingspan: 137 feet (41.8 meters) extended forward,
79 feet (24.1 meters) swept aft
Height: 34 feet (10.4 meters)
Weight: Empty, approximately 190,000 pounds (86,183 kilograms)
Maximum Takeoff Weight: 477,000 pounds (214,650 kilograms)
Speed: 600+ mph (Mach .92) @ 500 feet
825 mph (Mach 1.25) @ 50,000 feet
Rotate and Takeoff Speeds: 210 Gross - 119 Rotate kts / 134 kts Takeoff
390 Gross - 168 kts Rotate / 183 kts Takeoff
Landing Speeds: 210 Gross - 145 kts
380 Gross - 195 kts
Range: 7,455 miles, unrefueled
3,444 miles with normal weapons load
Ceiling: 60,000 feet (18,000 meters)
Crew: Four (aircraft commander, pilot, offensive systems officer and defensive systems officer)
Armament: NUCLEAR
CONVENTIONAL
84 Mk 62
84 MK82
30 CBU 87
30 CBU 89
30 CBU 97
12 Mk 65
PRECISION
30 WCMD
24 JDAM
12 GBU-27
12 AGM-154 JSOW
12 TSSAM
Unit Cost: $200 million per aircraft
http://www.globalaircraft.org/photos/planephotos/tornado_5.jpg
Tornado IDS
Length: 54' 10"
Height: 19' 4"
Wingspan: Fully forward: 45' 2", Swept: 27' 11"
Empty Weight: 30,620 lbs
Max Takeoff Weight: 61,620 lbs
Speed: Mach 2.2
Armament: Two Mauser 27mm cannons. 19,940 lbs of assorted air to air missiles, bombs, anti-radar and anti-ship missiles. Capable of carrying the B61 nuclear bomb.
Crew: 2
Cost: $26 million. 10% discount to regional allies.
Variable geometry, multirole aircraft designed more for ground strikes than air to air, though capable of handling both.
JF stands for Joint-Fighter
Upon customer request, the JF-20 can be fitted with Western weapons such as the Vulcan cannon, AIM-120 AMRAAM, AGM-65 Maverick, etc.
The aircraft has been developed in a 50-50 partnership with Dark terror's defence ministry, the BDIA, to meet a Bisonic frontal multi-role-fighter requirement, with a naval version (JF-20K) developed to meet the needs of a new plane for the Forcien and Bisonic Navies capable of performing both attack and air superiority missions. The aircraft has easily demonstrated manoeuvres yet to be emulated by any western aircraft.
Switchblade Wing Design
The wings are attached to its fuselage (body) at a pivot point toward the back of the plane. When the wings are fully extended, the plane can fly slowly to drop bombs precisely on their targets or land on short runways. When the wings are swept farther forward, the aircraft takes advantage of the maneuverability that forward-swept wings offer, and becomes an agile fighter. When the wings are swept fully forward, the trailing edge of the wing becomes the leading edge, and the aircraft turns into a delta shape perfect for dashing away at speeds up to Mach 3.
Armament
http://www.mach3graphics.com/misc%20graphics/jpg/SU-34%20ready.jpg
The JF-20 can carry up to 16 air-to-air missiles and up to 10000kg of ordnance. The fourteen external hardpoints can carry air-to-air missiles, air-to-surface missiles, bombs, rockets and an ECM (electronic countermeasures) pod. The aircraft is fitted with one Gsh-301 30mm gun with a maximum rate of fire of 1,500 rounds per minute.
The aircraft can be equipped with Vympel R-73E short-range air-to-air missiles with infrared terminal homing and RVV-AE long-range air-to-air missiles with active radar guidance. R-73E (NATO codename AA-11 Archer) is an all-aspect, close-combat missile capable of engaging targets in tail-chase or head-on mode at altitudes between 0.02 and 20km, and target g-load to 12g. The Vympel RVV-AE (AA-12 Adder) air-to-air missile, also known as the RR-77, can intercept targets at speeds up to 3,600kph and altitudes from 0.02 to 25km.
The Su-37 can be fitted with air-to-surface missiles such as the Kh-25 (AS-12 Kegler) short-range missile and Kh-29 (AS-14 Kedge) with a 317kg penetrating warhead, as well as air-launched versions of missiles such as the P-800 Yakhont (SS-N-26), Uran (SS-N-25 Switchblade), and Klub (SS-N-27), among others.
Sensors
Zhuk Multipurpose Radar
Range 175 miles. Can identify 60 targets and simultaneous track 30 target flying below
200ft while flying at 20,000ft.
E.S.M.: Radar detector, enables vehicle to detect other radars passively
Multi-target:
Can lock on and fire at up to 4 targets simultaneously with AA-13 missiles
V. A. S.: Amplify camera that allows targeting on fighter sized objects out to 30 miles
Targeting Laser/ Verifying Laser:
Used to target with laser guided weapons and to fly without using radar low to the ground
at night
the weapons management system, electronic warfare system and the Zhuk
radar work as one, giving the pilot unprecedented situation awareness.
Zhuk successfully detects air targets, manufactured with the use of "stealth" technology
The Zhuk radar is designed for air-superiority and strike operations and features a low observable, active aperture, electronically-scanned array with multi-target, all-weather capability.
The radar is key to the JF-20's integrated avionics and sensor capabilities. It will provide pilots with detailed information about multiple threats before the adversary's radar ever detects the JF-20. This is also called BVR, or Beyond Visual Range capability.
There are also systems for terrain-following and terrain-avoidance, mapping and multichannel employment of guided weapons
There is also a rear-looking NIIP NO-12 radar and optronic fire-control and surveillance system
Engines:
http://www.digikitten.com/playhousev2/files/pixelmonkey/zaengine.jpg
it uses Mach-3 G-50FU Pulse detonation engines for propulsion
the G-50FU pulse detonation engines are similar in size to modern turbojets (a bit smaller) but are more efficient because detonations create higher pressures and travel faster than turbojet combustion. This means more power, higher efficiency.
The 3-dimensional nozzle vectors thrust 20 degrees up down left and right for improved aircraft agility. This vectoring increases the roll rate of the aircraft by 50 percent and has features that contribute to the aircraft stealth requirements.
Heat-resistant components give the nozzles the durability needed to vector thrust, even in afterburner conditions.
With precision digital controls, the nozzles work like another aircraft flight control surface. Thrust vectoring is an integrated part of the Za-34's flight control system, which allows for seamless integration of all components working in response to pilot commands.
the G-50FU engines also feature:
Integrally bladed rotors: In most stages, disks and blades are made from a single piece of metal for better performance and less air leakage.
Long chord, shroud less fan blades: Wider, stronger fan blades eliminate the need for the shroud, a ring of metal around most jet engine fans. Both the wider blades and shroud less design contribute to engine efficiency.
Low-aspect, high-stage-load compressor blades: Once again, wider blades offer greater strength and efficiency.
Alloy C high-strength burn-resistant titanium compressor stators: innovative titanium alloy increases stator durability, allowing the engine to run hotter and faster for greater thrust and efficiency.
Alloy C in augmentor and nozzle: The same heat-resistant titanium alloy protects aft components, permitting greater thrust and durability.
Floatwall combustor: Thermally isolated panels of oxidation-resistant high cobalt material make the combustion chamber more durable, which helps reduce scheduled maintenance.
Fifth-generation full-authority digital electronic engine control (FADEC): Dual-redundant digital engine controls - two units per engine, two computers per unit - ensure unmatched reliability in engine control systems. The same experience that introduced full-authority digital control to fighter engines works with the aircraft system to make engine and aircraft function as a single flight unit.
No visible smoke: Reduces the possibility of an enemy visually detecting the JF-20.
Improved Supportability: All components, harnesses, and plumbing are located on the bottom of the engine for easy access, all line replaceable units (LRUs) are located one deep (units are not located on top of one another), and each LRU can be removed with just one of the six standard tools required for engine maintenance.
the JF-20 is a joint development between Dark terror and geforce4 of a new generation multi-role fighter.
The aircraft is being developed in a 50-50 partnership with Dark terror's defence ministry, to meet bisonic and forican naval multi-role-fighter requirements.
Cockpit:
http://www.digikitten.com/playhousev2/files/pixelmonkey/zacockpit.gif
The JF-20 features a side-stick controller in addition to two throttles that are the aircraft's primary flight controls. Located on the right console, the GEC-built stick also serves as a swing-out, adjustable arm rest. The stick is force sensitive and has a throw of only about one-quarter of an inch. The throttles are located on the left console.
During air combat, both the stick and the throttles are high-use controls . To support pilot functional requirements, the grips include buttons and switches (that are both shape and texture coded) to control more than 60 different time-critical functions. The buttons are used to control the offensive (weapons targeting and release) and defensive systems, (although some, like chaff and flares, can operate both automatically and manually) as well as display management.
The Heads Up Display or (HUD) server as the primary flight instrument for the pilot. It will have a viewable area of 30 degrees horizontally and 25 degrees vertically. Developed by the Air Force Instrument Flight Center, the GEC HUD will use standard symbology and be 4.5 inches in height. Unlike the HDD's, the GEC HUD will not be in color. However, the symbology will be exactly the same as the Head Down Displays. As a shock absorber from bird strikes, the windshield will be protected by a rubber buffer strip placed on the HUD combiner glass. During initial bird strike tests, the HUD would routinely shatter. Precautions were taken at all costs to avoid this from happening. The buffer strip would shield the polycarbonate glass by allowing it to flex during a strike. Design is underway for a collapsible HUD that would fall but not break. In addition, the JF-20 design also features a sort of laminate that eliminate glass from shattering in the cockpit.
The Integrated Control Panel (ICP) will be the main location where the pilot can manually input data for communications, autopilot and navigation. The ICP will be located below the HUD, underneath the glare shield and in the center top of the instrument panel. Additionally, the ICP will have "double click" features which are similar to a PC mouse in functionality. The double click feature will allow the pilot to input data more rapidly. Six Liquid crystal color displays will be housed in the cockpit. The LCD's will be fully readable in direct sunlight. Notable improvements of LCD's when compared to the older generation displays of CRT's are a lower weight, less size and a lower power consumption. The LCD's are inherently more reliable because of the lower power consumption. Two Up Front Display's (UFD)'s are located to the left and right of the ICP. They measure 3x4 inches. The primary function of the UFD's are to provide the pilot with cautionary information/warning/advisory, data communications/navigation/identification (CNI)data and act as the serve as the Stand-by Flight instrumentation Group and Fuel Quantity Indicator. A maximum of 12 messages can appear on the UFD's at any given time, and remaining faults can be indexed as sub pages.
http://www.mach3graphics.com/misc%20graphics/jpg/SU-30%20climb.jpg
http://www.mach3graphics.com/misc%20graphics/jpg/SU-30%20over%20Baikal.jpg
http://www.mach3graphics.com/misc%20graphics/jpg/SU-30MKK%20low%20level.jpg
http://www.mach3graphics.com/misc%20graphics/jpg/SU-34%20attack.jpg
Prices:
JF-20: $50 mil
JF-20K Naval Variant: $51 mil
JF stands for Joint-Fighter
Upon customer request, the JF-20 can be fitted with Western weapons such as the Vulcan cannon, AIM-120 AMRAAM, etc.
The aircraft has been developed in a 80-20 partnership with Dark terror's defence ministry.
cost: 45 million
JF-2000 Naval VSTOL fighter and attack aircraft
http://www.aeronautics.ru/img/img006/shafagh_iran_001.jpg
G-45FU VSTOL low-observable propulsion Engine:
http://www.digikitten.com/playhousev2/files/pixelmonkey/engtest.jpg
the G-45FU advanced propulsion system utilize cutting edge technology to provide the JF-2000 with higher performance than conventional fighter aircraft. The engine consists of a 3-stage fan, a 6-stage compressor, an annual combustor, a single stage high-pressure turbine, and a 2 stage low-pressure turbine.
The STOVL propulsion system is composed G-45FU engine and the lift fan system, 3BSD and roll posts.
The front of
G-45FU engine, for example, is only a few feet inside the air intake. To avoid radar
reflections, the engine face has been hidden by special inlet guide vanes that have been
treated with RAM and shaped to cause radar beams to make multiple bounces--including
onto the air-duct walls. There, radio-frequency energy is trapped by RAM or bounced
from interior surfaces, each time being greatly attenuated. One way or another, the radar
energy becomes too weak to constitute a dangerous reflection.
there are also an intake radar blocker built as part of the face of the engine with a
bullet-like centerpiece surrounded by angled, radiating vanes. and an
infrared and radar suppression devices for jet exhausts.
the engine is coupled with a shaft-driven lift fan system for STOVL propulsion. The lift fan has been developed by Rolls-Royce Defence. Doors installed above and below the vertical fan open as the fin spins up to provide vertical lift. The main engine has a three bearing swivelling exhaust nozzle. The nozzle, which is supplemented by two roll control ducts on the inboard section of the wing, together with the vertical lift fan provide the required STOVL capability.
http://www.aeronautics.ru/img/img006/shafagh_iran_003.jpg
Sokol Array Radar (it does not move):
http://www.digikitten.com/playhousev2/files/pixelmonkey/aejfsa.jpg
Sokol uses a non-equidistant rather than the traditional linear radar field distribution, which allows a fivefold radar cost reduction over a traditionally designed phased array radar. it has a 980mm antenna diameter (37dB gain) and weigh 275kg. The radar tracks 24-30 targets, engages the most dangerous 6 to 15 of them. Its electronic beam steering will give ±70 deg spatial coverage in both axes. Power output is 8kW peak, 2 - 3kW average. It is designed for high reliability, and is frequency agile with LPI and anti ECM features. It also incorporates target identification techniques, and it is capable of interleaving between air-to-air and air-to-ground modes.
Velocity search: 300km head-on vs fighter target.
Range-while-search, lookup mode: 180-210km head-on / 100km tail-on vs fighter target.
Range-while-search, lookdown mode : 200km head-on / 80km tail-on vs fighter target.
Track-while-scan mode: 250km head-on vs fighter target.
Against a large target such as a bomber or AWACS aircraft detection range comfortably exceeds 300km.
three radar arrays placed in the nose of the aircraft (one facing forward and two facing sideways). Each wing root carried an infrared search and track system that operated through faceted windows.
Cockpit:
http://www.digikitten.com/playhousev2/files/pixelmonkey/ef2000cock.jpg[img]
The cockpit in the JF-2000 is equipped with a touch-sensitive control display, a larger multi-purpose liquid crystal color display, which shows tactical information, two monochrome displays and a new engine fuel display. The aircraft retains the mission software and a high proportion of the avionics found in the C/D models.
The cockpit also has a color digital map and the pilots are equipped with night-vision goggles.
it also features HOTTAS and a collapsible HUD that would fall but not break.
The Heads Up Display or (HUD) will server as the primary flight instrument for the pilot. It will have a viewable area of 30 degrees horizontally and 25 degrees vertically.
The Integrated Control Panel (ICP) will be the main location where the pilot can manually input data for communications, autopilot and navigation. The ICP will be located below the HUD, underneath the glare shield and in the center top of the instrument panel. Additionally, the ICP will have "double click" features which are similar to a PC mouse in functionality. The double click feature will allow the pilot to input data more rapidly. 5 Liquid crystal color displays will be housed in the cockpit. The LCD's will be fully readable in direct sunlight.
SPECIFICATIONS
Payload: 9000 KG
Length 18.4 m
Height 4.6 m
Wing span 13.6 m
Maximum speed: mach 2.1
supercruise speed: mach 1.9
Internal AA cannon: 30mm GSh-30 twin-barrel aircraft cannon
maximum operational g-loading is 9g+.
[img]http://www.islamicdigest.net/albums/albun53/Shafaq.jpg
Weaponry
The design of the JF-2000 allows a rather large weapons bay capable of holding no less than 8 air-to-air missiles (AAM?s). The JF-2000's Maximum combat load is 9,000 kg , it can also carry 4 Kh-35 (SS-N-25 Switchblade) anti-ship missiles.
When backing up ground forces, the aircraft survivability is ensured by armour protection of the critical aircraft units (which is quite a problem for the aircraft type in question) as well as by the fact, that, provided low altitudes (less then 300m) and high speeds (more then 850 km/h), such an air target is rather hard to be engaged by enemy's ground AD forces
DesignThe JF-2000 is designed to have a reduced IR and Radar signature. This gives the aircraft the stealth capabilities. The JF-2000 is also designed, to be very light ,manoeuverable and with short take off and landing capabilities. The JF-2000 has a blended fuselage and a thick wing center-section. The aerodynamic configuration of the JF-2000 is considered to be very unusual and is equipped with powerful thrust vectoring system thus providing the aircraft with unimaginable agility. The landing gear of the JF-2000 is specially designed so as to allow landing approaches at high angle of attacks.
Supermaneuverability
The swivel wing panels with leading-edge flaps allows operation in the normal flow mode within the required fuselage orientation range. This provides a higher level of controllability in the supermaneuverability modes, elimination of an involuntary spin and entering the supermaneuverability mode at higher speeds. The wing panels at negative local angles temporally reduce the maximum wing load capacity and existing loads almost two-fold. Combined with an increased controllability, this gives the aircraft a possibility to maneuver not exceeding the permissible loads. The aircraft has a full-authority digital automatic control system with a thrust controlled engine nozzle included in the longitudinal and flight control systems. The above aerodynamic characteristics will ensure the aircraft's superiority in a short-time close combat, other things being equal.
Za-41 "FireFly" ASF
cost:40 million
http://www.digikitten.com/playhousev2/files/pixelmonkey/asf41.jpg
The Advanced Strike Fighter (ASF) is a multi-role stealthy strike fighter optimized for the air-to-ground role, designed to affordably meet the needs of the Air Force, Navy, and Marine Corps, with improved survivability, precision engagement capability, the mobility necessary for future joint operations and the reduced life cycle costs.
A notable design feature of this aircraft is the enhanced survivability. The cockpit is armor protected and pushrods are used in preference to cables for the flying control surfaces. The load bearing members are strengthened. The engines are widely separated and a 10 mm thick firewall is installed between them. The explosive resistant fuel tanks are filled with reticulated foam.
The aircraft has an all-welded 30 mm titanium alloy cockpit with transparent windscreen armor block to protect the pilot and is equipped with a single K-36L Zvezda ejection seat.
Cooling air is introduced at the end of the tailcone to reduce the temperature of the exhaust gasses and minimize the infrared signature of the aircraft.
The aircraft has a carrier-suitable tailhook. Its landing gear has a longer stroke and higher load capacity.
Other Special Features:
Survivability: radio frequency/infrared signature reduction and on-board countermeasures to survive in the future battlefield.
Lethality: integration of on- and off-board sensors to enhance delivery of current and future precision weapons
Supportability: reduced logistics footprint and increased sortie generation rate to provide more combat power earlier in theater
Affordability: focus on reducing cost of developing, procuring and owning ASF to provide adequate force structure
Heads Up Display
Hands-On Throttle and Stick (HOTAS)
Internal-Weapon Bays
Super-Cruise ability
"FireFly"Advanced Towed Decoys: These are mounted in two dispensers in the fighter's tail with two decoys in the dispenser on either wing. These drones are dragged about 328 feet (100 meters) behind the aircraft on a thin cable. Each is a specially designed radar lure that creates a radar image to mimic the aircraft. The decoy has a special jammer that is designed to decoy missiles that have been programmed to home on jamming signals. If decoys are not destroyed, they can be recovered and repaired.
ASF?s integrated avionics and stealth are intended to allow it to penetrate surface-to-air missile defenses to destroy targets, when enabled by air dominance. The ASF is designed to complement a force structure that includes other stealthy and non-stealthy fighters, bombers, and reconnaissance / surveillance assets.
The cockpit interior lighting is fully Night Vision Goggle (NVG) compatible, as is the exterior lighting. The cockpit panels feature extended life, self-balancing, electro luminescent (EL) edge-lit panels with an integral life-limiting circuit that runs the lights at the correct power setting throughout their life. It starts at one-half power and gradually increases the power output to insure consistent panel light intensity over time. As a result, the cockpit always presents a well-balanced lighting system to the pilot (there is not a mottled look in the cockpit). The panels produce low amounts of heat and power and are very reliable.
The aircraft also has integral position and anti-collision lights (including strobes) on the wings. The low voltage electro luminescent formation lights are located at critical positions for night flight operations on the aircraft (on the forward fuselage (both sides) under the chine, on the tip of the upper left and right wings, and on the outside of both vertical stabilizers. There are similar air refueling lights on the butterfly doors that cover the air refueling receptacle.
This aircraft packs state of the art sensors and communications equipment. Among it's many features is an enhanced radar system that can track up to 128 targets simultaneously out to a range of 250 miles (400 km). Any targets acquired by the radar are fed into the vehicle's targeting computers
the aircraft can fire missiles at up to 15 targets at the same time. It is also capable of Terrain Following for low altitude flight.
Stealth:
Radar Absorbing Material is covering the entire fuselage of the za-41. This material is made to absorb and kill radio waves instead of reflect
them.
the over-all shape of the aircraft has angles to it that scrambles the radar all over, everywhere but back to the radar's origin.
it also has special horizontal stabilizers located on the aft part of the aircraft. These stabilizers help evenly distribute the lift of the aircraft so that moisture Contrails are avoidable.
Specifications:
2 SKF-40E Pulse Detonation Engines with robust rotary valves [they use a two-stage ignition process to achieve detonation.]
detonation is a violent explosion and as such it produces vastly higher pressures than the simple burning process of deflagration.
Maximum Speed: Mach 4+
Supercruise speed: mach 3-3.2
ceiling: 110,000 ft
G-load: 9
range with external fuel tanks: 4,600 kilometres
Gun : one GSh-301
Ammunition 600 rounds
Firing rate 1,500 rounds per minute
Max Payload, 25,640 lb
Air-to-Air Missiles: up to 13
and large variety of Air-to-Surface Missiles including anti-ship
Bombs:laser-guided bombs and other advanced bombs.
Other: rocket pods, ECM pods
Please note:
Dealer and manufacturer (production) rights are reserved to Geforce4 only!
Thank you for your understanding.©
Ezh-444MCA Multi-Sensor Command and Control Aircraft [ AESA equiped ]
cost: 800 million credits
http://www.boeing.com/news/feature/concept/images/010426a.jpg
Ezh-444MCA is an aircraft that could support capabilities currently delivered by AWACS, Joint STARS, and the Airborne Command and Control Center all Together!, it provides the military with an aircraft capable of serving as an intelligence, surveillance and reconnaissance (ISR) platform fully interoperable with other aircraft and unmanned systems.
Specifications:
Environmental benefits include landings and takeoffs quieter than Stage 4 airplanes and the same fuel burn as today's best performers.
http://www.boeing.com/news/feature/concept/images/k61686.jpg
Maximum cruising Altitude: Mid-40,000-foot level or higher (13,000 meters+)
Coverage 360º air and maritime
Tracking capability more than 3500 targets
Crew: Two flight crew and up to 10 mission crew
Range: Between 6,000 and 9,000 nautical miles
Max Speed: mach 1.1
Endurance: 25 hours, with 800 km radius of action
Cockpit: http://www.airforce-technology.com/projects/737aewc/images/737AEWC_3.jpg
Ezh-444 Tanker Version
cost: 40 million
http://www.boeing.com/news/feature/concept/images/concept.jpg
it can itself be refueled in flight. It also have the capability to refuel Air Force, Navy, Marine and other aircraft on every mission!.
Equipped with both the proven boom-and-receptacle and the hose-and-drogue aerial refueling systems, the Ezh-444 Tanker/Transport offers maximum operational flexibility, Ezh-444 Tanker/Transport is really four aircraft in one. While maintaining its tanker capability, the aircraft's uninterrupted cabin floor can be configured for: Passenger; Freighter; Convertible (passenger or freighter); and Combi (passenger and freighter).
The installation of wingtip refuelling pods involves a major modification and refit to the entire aircraft, including modifications to the wing and fuselage fuel tanks, additional fuel control systems and the installation of indicators and circuit breakers on the flight deck.
Inside the refuelling pods, a collapsible funnel-shaped drogue is attached to a hose, which is reeled out to trail behind the wing of the aircraft. The hose is fitted with a constant tension spring to give stability to the hose while it is extended.
Orel AEW&CS aircraft
cost: 270 million
http://www.spyflight.co.uk/images/JPGS/Boeing%20707/707%20Condor%20port.jpg
http://www.spyflight.co.uk/images//JPGS/Boeing%20707/707%20Condor%20starboard.jpg
http://www.spyflight.co.uk/images/JPGS/Boeing%20707/phalcon.jpg
The world's most advanced AEWC&C system, the OREL, was developed and produced by Geforce using Active Phased Array Electronic Scanning Technology rather than a mechanically rotating antenna (rotodome) used by current AWACS systems, giving OREL greater operational flexibility and performance by several orders of magnitude. The Orel AEW&C aircraft is based on four sensors: phased-array radar, phased-array IFF, ESM/ELINT and CSM/COMINT. A unique fusion technology continuously cross-relates the data gathered by all sensors. When one of the sensors reports a detection, the system automatically initiates an active search of the complementary sensors.
The AWE&C phased array radar replaces the conventional rotodome radar. It is mounted either on the aircraft fuselage or on top of the aircraft inside a stationary dome, providing full 360° coverage. This electronically steered beam radar delivers a tremendous advantage over mechanical rotating antenna, as it supports the tracking a high maneuvering targets. The radar can detect even low flying objects from distances of hundreds of kilometers, day and night, under all weather conditions. Verification beams sent at specific, individual, newly detected targets eliminate false alarms. Moreover, track initiation is achieved in 2 to 4 seconds as compared to 20 to 40 seconds with a rotodome radar
The IFF system employs solid state phased array technology to perform interrogation, decoding, target detection and tracking. A monopulse technique is used to implement azimuth measurement. The IFF data is automatically correlated with the phased array radar.
The ESM/ELINT system receives, analyzes and locates radar signals, covering 360o. It combines high sensitivity with high probability of intercept, and achieves excellent accuracy in bearing measurement. The system uses narrow-band super-heterodyne receivers and wide-band instantaneous frequency measurement (IFM) techniques to provide very high accuracy and probability of intercept of airborne and surface emitters. Very high bearing accuracy for all received signals is achieved through Differential Time of Arrival (DTOA) measurements. The system also collects and analyzes ELINT data.
The Orel's CSM/COMINT receives in UHF, VHF and HF, rapidly searching for airborne, shipborne or ground communications signals of interest. Selected radio nets can be monitored for signal activity. A DF capability locates targets. Detected signals can be assigned to monitoring receivers instantaneously. The system makes extensive use of computers to reduce the load on operators.
specifications:
Wing Span: 44.60 m
Wing Area: 283.40 m²
Length: 44.40 m
Height: 12.90 m
Engine 4 x P&W JT3D-3B
Maximum speed: 973 Km/h
Range 6,920 Km
Primary Radar
Type electronically scanned array, all weather
Frequency L-band
Coverage 360º air and maritime
Range more than 300nm
IFF range 400nm
Tracking capability more than 2700 targets
Multi role mission consoles 5
naval AWACS Orel-45
cost: 120 million
http://homepage.tinet.ie/%7Esteven/images/hawkeyefr8.jpg
The AN/AGPS-170 radar is capable of tracking more than 2,000 targets and controlling the interception of 70 hostile targets. One radar sweep covers 6 million cubic miles. The radar's total radiation aperture control antenna reduces sidelobes and is robust against electronic countermeasures. It is capable of detecting aircraft at ranges greater than 550km.
The mission computer is equipped with an enhanced high-speed parallel processor. advanced display system and computer peripherals provide the operators with multicolour displays, map overlays, zoom facilities and auxiliary data displays.
Secondary roles of the Orel-45 include strike command and control, surveillance as well as guidance of search and rescue missions
Specification:
Cruise speed, km/h 750
Range 500 km with 6 hr 30 min on station
Endurance 6 hr 15 min
Detection range of aircraft greater than 550 km
HELICOPTERS
AH-64A/D Apache Attack Helicopter
http://www.military.com/Data/EQG/ah64_large.jpg
http://www.fas.org/man/dod-101/sys/ac/ah-64d-image25.jpg
This is the battle tested Apache available in standard and Longbow variants. Both have one M230 30mm gun and can carry 70mm (2.75 inch) Hydra-70 folding-fin rockets, up to 16 AGM-114 Hellfire anti-tank missiles, AGM-122 Sidearm anti-radar missiles, AIM-9 Sidewinder or FIM-92 Stinger air-to-air missiles, and have nightvision and low-light vision systems standard. The Longbow comes complete with advanced targeting systems, a mushroom shaped powerful radar, and the ability to carry Hellfire MMW air to surface/air to air missiles.(Longbow shown in image)
Max speed is 163 knots
Crew is 2
Each AH-64A Apache costs $15.4 million
Each AH-64D Longbow costs $17.2 million
AH-64A Apache Attack Helicopter
http://s3.invisionfree.com/Jaxusism/index.php?act=Attach&type=post&id=3977
Propulsion Two T700-GE-701Cs
Crew Two
Length 58.17 ft (17.73 m) 58.17 ft (17.73 m)
Height 15.24 ft (4.64 m) 13.30 ft (4.05 m)
Wing Span 17.15 ft (5.227 m) 17.15 ft (5.227 m)
Primary Mission Gross Weight 15,075 lb (6838 kg)11,800 pounds Empty 16,027 lb (7270 kg) Lot1
Weight Hover In-Ground Effect (MRP) 15,895 ft (4845 m)
Hover Out-of-Ground Effect (MRP) 12,685 ft (3866 m)
Maximum Level Flight Speed 150 kt (279 kph)
Range 400 km - internal fuel 1,900 km - internal and external fuel
Armament: Primary MissionStarboard WingM230 GunPort WingRate of ClimbDurationCombat (Anti-armor)
4 Hellfire320 rds 30mm
4 Hellfire1450 fpm1.8 hours
Multi-role (Covering force)
4 Hellfire 19 FFAR *1200 rds 30mm
4 Hellfire 19 FFAR *860 fpm2.5 hours
Close-support (Anti-armor)
8 Hellfire1200 rds 30mm
8 Hellfire990 fpm2.5 hours
Ground-support (Airmobile escort)38 FFAR *1200 rds 30mm38 FFAR *780 fpm2.5 hours
M230 33mm Gun
70mm (2.75 inch) Hydra-70 Folding-Fin Aerial Rockets
AGM-114 Hellfire anti-tank missiles
AGM-122 Sidearm anti-radar missile
AIM-9 Sidewinder Air-to-Air missiles
Unit Cost: $23 Million
MISSILES
AIM-9 SIDEWINDER
http://www.af.mil/media/factsheet/aim_9.jpg
FEATURES
The AIM-9 has a cylindrical body with a roll-stabilizing rear wing/rolleron assembly. Also, it has detachable, double-delta control surfaces behind the nose that improve the missile's maneuverability. Both rollerons and control surfaces are in a cross-like arrangement.
The missile's main components are an infrared homing guidance section, an active optical target detector, a high-explosive warhead and a rocket motor.
The infrared guidance head enables the missile to home in on target aircraft engine exhaust. An infrared unit costs less than other types of guidance systems, and can be used in day/night and electronic countermeasures conditions. The infrared seeker also permits the pilot to launch the missile, then leave the area or take evasive action while the missile guides itself to the target.
General Characteristics
Primary Function: Air-to-air missile
Power Plant: Hercules and Bermite Mk 36 Mod 11
Length: 9 feet, 5 inches (2.87 meters)
Diameter: 5 inches (0.13 meters)
Finspan: 2 feet, 3/4 inches (0.63 meters)
Warhead: Annular blast fragmentation warhead
Launch Weight: 190 pounds (85.5 kilograms)
Guidance System: Solid-state, infrared homing system
Unit Cost: Approximately $84,000
AGM-88 HARM
http://www.af.mil/media/factsheet/agm88.jpg
FEATURES
The AGM-88 can detect, attack and destroy a target with minimum aircrew input. The proportional guidance system that homes in on enemy radar emissions has a fixed antenna and seeker head in the missile nose. A smokeless, solid-propellant, dual-thrust rocket motor propels the missile. The F-16C has the capability to employ the AGM-88, and is the only aircraft in the current inventory to use the AGM-88.
General Characteristics
Primary Function: Air-to-surface anti-radiation missile
Thrust: Dual thrust
Length: 13 feet, 8 inches (4.14 meters)
Launch Weight: 800 pounds (360 kilograms)
Diameter: 10 inches (25.40 centimeters)
Wingspan: 3 feet, 8 inches (101.60 centimeters)
Range: 30 plus miles (48 plus kilometers)
Speed: Supersonic
Aircraft: Used aboard the F-16C
Guidance System: Proportional
Warheads: High explosive
Unit Cost: $200,000
JAXMi2 Missiles : VERY explosive missiles. One missile capable of destroying an entire CITY! How did they come to be? An unidentified liquid was found and tested and found to be extremely explosive. More information on JAXMi2 Here (http://www.nationstates.net/forum/viewtopic.php?t=89886)!
Cost : $1 billion USD EACH
AIM-120 AMRAAM
http://www.af.mil/media/factsheet/aim120.jpg
FEATURES
The AMRAAM program improves the aerial combat capabilities of U.S. and allied aircraft to meet current and future threat of enemy air-to-air weapons. AMRAAM is compatible with the Air Force F-15, F-16 and developmental F-22; Navy F-14 D/D (R) and F/A-18 C/D; German F-4 and the British Sea Harrier aircraft.
AMRAAM is a follow-on to the AIM-7 Sparrow missile series. The missile is faster, smaller and lighter, and has improved capabilities against low-altitude targets. It incorporates active radar with an inertial reference unit and micro-computer system, which makes the missile less dependent upon the fire-control system of the aircraft. Once the missile closes on a target, its active radar guides it to intercept. This enables the pilot to aim and fire several missiles simultaneously at multiple targets. The pilot may then perform evasive maneuvers while the missiles guide themselves to their targets.
General Characteristics
Primary Function: Air-to-air tactical missile
Length: 143.9 inches (366 centimeters)
Launch Weight: 335 pounds (150.75 kilograms)
Diameter: 7 inches (17.78 centimeters)
Wingspan: 20.7 inches (52.58 centimeters)
Range: 20+ miles (17.38+ nautical miles)
Speed: Supersonic
Guidance System: Active radar terminal/inertial midcourse
Warhead: Blast fragmentation
Unit Cost: $386,000
AIM-7 SPARROW
http://www.af.mil/media/photodb/web/web_030819-F-8888Z-003.jpg
FEATURES
The missile has four major sections: guidance section, warhead, control and rocket motor. It has a cylindrical body with four wings at mid-body and four tail fins. Although external dimensions of the Sparrow remained relatively unchanged from model to model, the internal components of newer missiles represent major improvements with vastly increased capabilities.
General Characteristics
Primary Function: Air-to-air guided missile
Length: 12 feet (3.64 meters)
Diameter: 8 inches (0.20 meters)
Wingspan: 3 feet, 4 inches (1 meter)
Warhead: Annular blast fragmentation warhead
Launch Weight: Approximately 500 pounds (225 kilograms)
Guidance System: Raytheon semiactive on either continuous wave or pulsed Doppler radar energy
Unit Cost: $125,000
JOINT DIRECT ATTACK MUNITIONS GBU 31/32
http://www.af.mil/media/factsheet/jdam.jpg
FEATURES
JDAM is a guided air-to-surface weapon that uses either the 2,000-pound BLU-109/MK 84 or the 1,000-pound BLU-110/MK 83 warheads as the payload. JDAM enables employment of accurate air-to-surface weapons against high priority fixed and relocatable targets from fighter and bomber aircraft. Guidance is facilitated through a tail control system and a GPS-aided INS. The navigation system is initialized by transfer alignment from the aircraft that provides position and velocity vectors from the aircraft systems.
Once released from the aircraft, the JDAM autonomously navigates to the designated target coordinates. Target coordinates can be loaded into the aircraft before takeoff, manually altered by the aircrew before weapon release, and automatically entered through target designation with onboard aircraft sensors. In its most accurate mode, the JDAM system will provide a weapon circular error probable of 13 meters or less during free flight when GPS data is available. If GPS data is denied, the JDAM will achieve a 30-meter CEP or less for free flight times up to 100 seconds with a GPS quality handoff from the aircraft.
JDAM can be launched from very low to very high altitudes in a dive, toss and loft or in straight and level flight with an on-axis or off-axis delivery. JDAM enables multiple weapons to be directed against single or multiple targets on a single pass.
JDAM is currently compatible with B-1B, B-2A, B-52H, F-15E, F-14A/B/D, F/A-18E/F, F-16C/D and F/A-18C/D aircraft. Follow-on integration efforts are currently underway or planned to evaluate compatibility with the A-10, F/A-22, F-117, AV-8B, S-3, and the Joint Strike Fighter.
General Characteristics
Primary Function: Guided air-to-surface weapon
Length: (JDAM and warhead) GBU-31 (v) 1/B: 152.7 inches (387.9 centimeters); GBU-31 (v) 3/B: 148.6 inches (377.4 centimeters); GBU-32 (v) 1/B: 119.5 inches (303.5 centimeters)
Launch Weight: (JDAM and warhead) GBU-31 (v) 1/B: 2,036 pounds (925.4 kilograms); GBU-31 (v) 3/B: 2,115 pounds (961.4 kilograms); GBU-32 (v) 1/B: 1,013 pounds (460.5 kilograms)
Wingspan: GBU-31: 25 inches (63.5 centimeters); GBU-32: 19.6 ins. (49.8 centimeters)
Range: Up to 15 miles
Ceiling: 45,000-plus feet (13,677 meters)
Guidance System: GPS/INS
Unit cost: Approximately $21,000 per tailkit
LG-118A PEACEKEEPER
http://www.af.mil/media/factsheet/lg118.jpg
FEATURES
The Peacekeeper is capable of delivering 10 independently targeted warheads with greater accuracy than any other ballistic missile.. It is a four-stage rocket ICBM system consisting of three major sections: the boost system, the post-boost vehicle system and the re-entry system.
The boost system consists of four rocket stages that launch the missile into space. These rocket stages are mounted atop one another and fire successively. Each of the first three stages exhausts its solid propellant materials through a single movable nozzle that guides the missile along its flight path.
Following the burnout and separation of the boost system's third rocket stage, the fourth stage post-boost vehicle system, in space, maneuvers to deploy the re-entry vehicles in sequence.
The post-boost vehicle system is the Peacekeeper Stage IV that has a guidance and control system and re-entry system. The post-boost vehicle rides atop the boost system, weighs about 2,500 pounds (1,333 kilograms) and is 3.5 feet (1.07 meters) long.
The top section of the Peacekeeper is the re-entry system. It consists of the deployment module, up to 10 cone-shaped re-entry vehicles and a protective shroud. The shroud protects the re-entry vehicles during ascent. It is topped with a nose cap, containing a rocket motor to separate it from the deployment module.
The deployment module provides structural support for the re-entry vehicles and carries the electronics needed to activate and deploy them. The vehicles are covered with material to protect them during re-entry through the atmosphere to their targets and are mechanically attached to the deployment module. The attachments are unlatched by gas pressure from an explosive cartridge broken by small, exploding bolts, which free the re-entry vehicles, allowing them to separate from the deployment module with little disturbance. Each deployed re-entry vehicle follows a ballistic path to its target.
General Characteristics
Primary Function: Strategic deterrence
Warheads: 10
Load: Avco MK21 re-entry vehicles
Guidance System: Inertial; integration by Boeing North American, IMU by Northrop and Boeing North American
Thrust: First stage, 500,000 pounds
Length: 71 feet (21.8 meters)
Weight: 195,000 pounds (87,750 kilograms) including re-entry vehicles
Diameter: 7 feet, 8 inches (2.3 meters)
Range: Greater than 6,000 miles (5,217 nautical miles)
Speed: Approximately 15,000 miles per hour at burnout (Mach 20 at sea level)
Unit Cost: $70 million
LGM-30 MINUTEMAN III
http://www.af.mil/media/photodb/web/web_030813-F-8888U-005.jpg
FEATURES
The Minuteman is a strategic weapon system using a ballistic missile of intercontinental range. Missiles are dispersed in hardened silos to protect against attack and connected to an underground launch control center through a system of hardened cables. Launch crews, consisting of two officers, perform around-the-clock alert in the launch control center.
A variety of communication systems provide the president and secretary of defense with highly reliable, virtually instantaneous direct contact with each launch crew. Should command capability be lost between the launch control center and remote missile launch facilities, specially configured E-6B airborne launch control center aircraft automatically assume command and control of the isolated missile or missiles. Fully qualified airborne missile combat crews aboard airborne launch control center aircraft would execute the president's orders.
An extensive life extension program is under way to keep the missiles safe, secure and reliable well into the 21st century. These major programs include: replacement of the aging guidance system, remanufacture of the solid-propellant rocket motors, replacement of standby power systems, repair of launch facilities, and installation of updated, survivable communications equipment, and new command and control consoles to enhance immediate communications.
General Characteristics
Primary Function: Intercontinental ballistic missile
Length: 59.9 feet (18 meters)
Weight: 79,432 pounds (32,158 kilograms)
Diameter: 5.5 feet (1.67 meters)
Range: 6,000-plus miles (5,218 nautical miles)
Speed: Approximately 15,000 mph (Mach 23 or 24,000 kph) at burnout
Ceiling: 700 miles (1,120 kilometers)
Thrust: First stage, 202,600 pounds
Load: Re-entry vehicle: Lockheed Martin Missiles and Space MK 12 or MK 12A
Guidance systems: Inertial system: Boeing North American; ground electronic/security system: Sylvania Electronics Systems and Boeing Co.
Unit cost: $7 million
RIM-7 SEA SPARROW
http://globalsecurity.org/military/systems/munitions/images/seasparrow-atsea39-s.jpg
POWEer Plant Hercules MK-58 solid-propellant rocket motor
Thrust Classified
Speed More than 2,660 mph (4,256 kph)
Range More than 30 nautical miles (approximately 55 km)
[Maximum Range = 6 nm according to other sources]
Minimum Range - 1600 yards
Director Lock-on Range - 50 nautical miles
Length 12 feet (3.64 meters)
Diameter 8 inches (20.3 cm)
Wingspan 3 feet 4 inches (one meter)
Warhead Annular blast fragmentation warhead, 90 pounds (40.5 kg)
Proximity fuzed, continuous expanding rod, with a 27 ft. kill radius
fire control systems MK 91
Launch Platform (Launcher) MK 29 Mod 1.
Launch Weight Approximately 500 pounds (225 kg)
Guidance System Raytheon semi-active on continuous wave or pulsed Doppler radar energy
Date Deployed 1976
Unit Cost $165,400
BGM-109 Tomahawk
http://www.fas.org/man/dod-101/sys/smart/slcm-dvic470.jpg
Length: 18 feet 3 inches (5.56 meters); with booster: 20 feet 6 inches (6.25 meters)
Weight: 2,650 pounds (1192.5 kg); 3,200 pounds (1440 kg) with booster
Diameter: 20.4 inches (51.81 cm)
Wing Span (when deployed): 8 feet 9 inches (2.67 meters)
Range: Land attack, conventional warhead: 600 nautical miles
Speed: Approx. 550 mph
Warheads: Conventional 1000 lb high explosive warhead OR conventional munition bomblet dispenser OR 200 kiloton W-80 nuclear warhead. Comes with standard high explosive warhead.
Cost: $750,000
Launched from the sea via a torpedo tube, Vertical Launch System, or Armored Box Launcher, this highly destructive, highly accurate, and highly versatile missile has been the main land attack missile of the American navy for the last decade. It is also highly accurate, with only a handful of booster failures in its history, and a 90%+ strike success rate in both Iraq and Bosnia. Great addition to any navy.
NAVAL
SSN-21 SEA WOLF SUBMARINE
http://globalsecurity.org/military/systems/ship/images/ssn-21-dvic117-s.jpg
Builders General Dynamics Electric Boat Division
Power Plant One S6W reactor
one shaft at with 52,000 shp with pumpjet propulsor
Improved Performance Machinery Program Phase II one secondary propulsion submerged motor
Length 353 feet (107.6 meters)
Draft 35 feet (10.67 meters)
Beam 40 feet (12.2 meters)
Displacement 7,460 ton surface displacement
9,137 tons submerged displacement
Speed Official: 25+ knots (28+ miles per hour, 46.3+ kph)
Actual: 35 knots maximum submerged speed
Actual: 20 knots tactical ["silent"] speed
Operating Depth Official: "greater than 800 feet"
Actual: About 1600 feet
Jane's Fighting Ships: 2000 feet
Armament eight 660-mm torpedo tubes
50 Tomahawk cruise missiles or
50 Harpoon antiship missiles or
50 Mark 48 ADCAP torpedoes or
up to 100 mines Systems AN/BSY-2 active-passive Sonar/Fire Control w/
hemispherical bow array and wide aperture array
TB-16B or TB-23 towed array
AN/BPS-16 search and navigation radar
AN/WLQ-4(V)1 ES receiver
Central Combat System (CCS) MK2
Link 11 Tactical data link
OTCIXS Tactical data link
Crew 12 Officers; 121 Enlisted
Price : 900million
JAX Modified IOWA-CLASS Battle Ship
http://globalsecurity.org/military/systems/ship/images/missour2-s.jpg
length:888ft
beam:109ft
draft:38ft
max speed:35knots
powerplants:8boilers,4geared turbines,4shafts,212,000shaft horse power.
Armament 32 - Tomahawk ASM/LAM - 8 armored box launchers
16 - Harpoon ASM - 4 quad cell launchers
9 - Mk 7 - 16-inch / 50 caliber guns
12 - Mk 28 - 5-inch / 38 caliber guns
4 - Mk 15 - 20mm Phalanx CIWS
Combat Systems SPS-49 Air Search Radar
SPS-67 Surface Search Radar
4 Mk37 Gun Fire Control
2 Mk38 Gun Direction
1 Mk40 Gun Director
1 SPQ-9 [BB-61] SLQ-25 NIXIE
SLQ-32 EW system
Aircraft None embarked
landing area and unhangared parking area
4 SH-3 or
4 SH-60
Crew : 65officers, 1450 enlisted, 58marines.
Price : 4 billion