The Macabees
03-03-2005, 03:22
[NOTE: Yea, Luftkrieg probably means nothing in German. I can care less. It was just a name.]
RULES
1. Do not ask for production rights. If you really, really, want them send me a telegram and make your offer – but beware, I won’t sell them cheap (in the billions).
2. I can do your math, but I would appreciate it if you would do it yourself.
3. All of these designs have those magic sensors which everyone adds if you try to copy them. If you do copy them and use/sell them I will be knocking on your frontdoor.
4. Don’t clog my thread with criticism. Telegram me if you want to say something, or have a problem with something.
DISCOUNTS
25% discount for allies – if you’re on this (http://forums.jolt.co.uk/showthread.php?t=401190) list you’re good. Does not include Naram-Sin.
10% discount for orders over twenty-five billion.
30% discount for regular costumers. These are people on the following list:
Mekugi
----------------------------------
NOTE: 2005 - 2010
MMA-A3 Falcon
It's termed here as the Su-63 because that's the Malatose designation and he wrote it up as the rest of us gave him the information - he as well gave massive input on the actual design.
With the growing Airforces of the world the Macabee and Malatose Governments decided to come together in this joint effort to create a Air Superiority Fighter beyond the rest.This Fighter was designed to win the skies with its advanced Avionic Systems and to develop precision ground strikes against targets.
The Su-63 FireStorm Air Superiority Fighter.[/i]
[b]STATISTICAL DATA:
HEIGHT:
6.3 m
WINGSPAN:
15.2 m
LENGTH:
22.0m
Engines:
2 x SATURN/LYU'KA AL-67 turbo fan engines with thrust-vectoring nozzles providing STOL capabilities, 160 kN static thrust with 250 kN of afterburner.
FUEL CAPACITY:
2,300 US gal (8,706 liters)
MAXIMUM SPEED @ 14,500 meter :
Mach 2.8
CRUISE SPEED (max performance without afterburner):
1805 kph (Mach 1.7)
STALL SPEED:
120 kph
CLIMB RATE:
28,000 meters per minute
CEILING:
20,000 meters (65 kft)
MIN LANDING DISTANCE AT SEA LEVEL:
300 meters
MAX COMBAT RADIUS:
2500 km
MAX RANGE (without external stores):
5600km
ESTIMATED COST:
$195,000,000
---------
Weapons Systems
2 x One GSh-30-1 30mm: Two GSh-30-1 30-mm cannons are mounted in blisters on either side of the main fuselage. The cannons are mounted on a geared rotor that is driven by a 20-hp electric motor which turns the barrels while each one fires individually. The cannon is capable of firing up to 7,200 rounds per minute with a muzzle velocity of 1,030 meters per second. Each cannon is fed from an internal 800 round storage drum which feeds the cannon with a double-ended hydraulically driven linkless feed system.
13 x BODY/WING HARD POINTS: 25,000 lb (11,340 kg) of external stores can be mounted on six hard points mounted on either wing and four under the main fuselage.
2 Internal Hardpoints: Internal Hardpoints can carry over 2,000lb of Internal Stores,such as bombs or 2 Missiles.
Cockpit
http://img18.exs.cx/img18/6537/cockpit0016ox.gif
The Cockpit of the Su-63 is all glass.There are no traditional round dial, standby or dedicated gauges and the Cockpit is fully Night Vision Compatible.
The GEC-built Head-Up Display (HUD) offers a wide field of view (30 degrees horizontally by 25 degrees vertically) and serves as a primary flight instrument for the pilot.
There are six liquid crystal display (LCD) panels in the cockpit. These present information in full color and are fully readable in direct sunlight. LCDs offer lower weight and less size than the cathode ray tube (CRT) displays used in most current aircraft. The lower power requirements also provide a reliability improvement over CRTs. The two Up-Front Displays (UFDs) measure 3"x4" in size and are located to the left and right of the ICP
The Integrated Control Panel (ICP) is the primary means for manual pilot data entry for communications, navigation, and autopilot data. Located under the glareshield and HUD in center top of the instrument panel, this keypad entry system also has some double click functions, much like a computer mouse for rapid pilot access/use.
The Primary Multi-Function Display (PMFD) is a 8"x8" color display that is located in the middle of the instrument panel, under the ICP. It is the pilot’s principal display for aircraft navigation (including showing waypoints and route of flight) and Situation Assessment (SA) or a "God's-eye view" of the entire environment around (above, below, both sides, front and back) the aircraft.
Three Secondary Multi-Function Displays (SMFDs) are all 6.25" x 6.25" and two of them are located on either side of the PMFD on the instrument panel with the third underneath the PMFD between the pilot's knees. These are used for displaying tactical (both offensive and defensive) information as well as non-tactical information (such as checklists, subsystem status, engine thrust output, and stores management).
CockPit Electronics
2 task-switching MFDs
Multi-node radar indication panel
Octo-functional HUD synchronized with MFD and helmet targeting
GPS synchronization panel
Topographic orientation TRV systems
Autopilot TRV/NRT based systems
JTIDs/A50 airbourne intelligence/global targetting, guidance systems.
APEX 345 ejection seat, syncronized with primary turbine faliures.
LIDAR/RADAR incoming signal indicator/interceptor to JTIDs.
--
Maneuvering System
The Sukhoi Su-63 is an extremely maneuverable fighter using 3D thrust vectoring and an innovated reverse canard design.The Su-63 uses an extensive fly-by-wire system which gives the pilot unprecedented abilities in piloting the aircraft.
Avionics.
The Su-63 uses advanced integrated Avionic Systems developed jointly by Finnish and Soviet Scientist.These systems computing power are equal to that of 7 Cray Super Computers.
--
ACTIVE SENSOR JAMMER: Internal ECM providing broadband RF protection.
AUTO-PILOT: The Su-63 is equipped with a computerized auto-pilot, allowing the pilot to relax or even sleep during long voyages. The auto- pilot can be programmed with a single destination or a complex flight plan involving multiple speeds, directions, and destinations. The onboard computer will alert the pilot when the fighter is near its destination.
OPTICS (NIGHTVISION):100km range. A passive light image intensifier that emits no light of its own, but relies on ambient light which is electronically amplified to produce a visible picture.
NO-12M: Multi-mode X-band pulse Doppler radar. Detection Range is 250km. System consists of a single electronically-scanned Phased-Array RADAR antenna mounted in the nose and tail giving the Su-63 360 degree scanning capabilites.System can track 50 Targets and simultaeneously fire at 5.The NO-12M RADAR can also be integrated with AWAC or ground based RADAR systems to give it a total detection range of 700km.
NO-15M Infra-Red Sensor System: Scans for enemy heat signatures at a range of up to 110km.
NLTS Laser Targeting system: Has a range of 50 km and is used to increase the accuracy of onboard weapons.
NOLDR(LIDAR system): The NOLDR is a heterodyne-reception optical radar system which uses pulse-tone waveforms.The system also uses Doppler RADAR.It reduces backscattering and extinction of coefficient of the atmosphere.
NO-Z2M Intra-Data Link System: Allows for all Su-63 Fighterstorm Fighters to share information automatically without radio calls.The wing leader can also easily glance at the computer and tell how much fuel and weapons his wingmen have left.He can also see which enemy fighter his wingman has targeted.This system allows for the wing commander to assign targets to each of his wingmen also.
RADIO/VIDEO COMMUNICATION: Long range, directional communications system with satellite relay capabilities. Range: 600 miles (960 km) or can be boosted indefinitely via satellite relay.
TACTICAL LIFE SUPPORT SYSTEM: The Su-63 pressurized and provides full nuclear and chemical protection.
--
Stealth Technology
The Su-63 employs technologies to significantly reduce Radar Cross Section (RCS), infrared signature, electromagnetic signature, visual signature and aural signature. RCS reduction represents the paramount LO feature considered in the Su-63 design. To reduce RCS, the
S-63 employs a geometrically based radar disbursing configuration. Developed utilizing computational RCS modeling techniques employed and/or developed by Sukhoi, the Su-63 configuration employs facets approximated by curvelinear, polynomial sections. Ultimate Su-63 RCS reduction, however, is dependent upon a proprietary combination of bandpass external skins, internal shaping and the implimentation of Cold-Plasma-Cavity Active Stealth Technology. Between the external bandpass skins and the internal graphite hull backed by an alloy geodetic structure is a cavity. Within this cavity a low temperature plasma is achieved. This plasma, as manipulated actively by the aircraft’s computer driven self-protection network, provides an unparalleled level of active stealth technology whereby incoming interrogative radar energy is substantially disrupted such that return signal is mitigated to undetectable levels or chaotic, undeciferable signals. Rather than rely solely upon external shaping, Sukhoi proprietary Su-63 stealth technology adapts to frequency and bandwidth, allowing maximum LO performance against all air-to-air and ground based radar types alike. Su-63 clean, all-aspect RCS is on the order of 0.006 square meters.
To reduce RCS while carrying external stores, the aircraft can be equipped with Radar Elusive Tactical Stores Dispensers (RETSD™), developed by Sukhoi. These dispensers allow the Su-63 to carry wing mounted external stores without compromising LO features. This allows the Su-63 to conduct precision strike and air-to-air engagements with limited detectability. The Su-63 also features two independent, internal weapons bays for compact internal stores carriage including both the tube-launched short range AAM as well as 250 LB class precision guided munitions. Carriage of compact stores within these internal weapons bays permits a slightly armed Su-63 to function in a "clean" RCS configuration.
Reduction of IR emissions is achieved through the use of a dedicated engine bay cooling/IR signature reduction system. Ducting residual inlet air through the Powerplant Signature Reduction Shroud (PSRS), significantly reduces aircraft IR signature both in the subsonic and supersonic regime. Coupled with Lo-Axi™ or similar LO turbofan exhaust nozzle, the aircraft IR signature is substantially reduced.
Aural signature is reduced in part through the PSRS. For enhanced aural signature reduction, Sukhoi is considering Active Frequency Damping (AFD) and comparable active noise control systems. Visual signature is reduced through employment of smokeless turbofans and by limiting overall aircraft size.
Protection against Scalar EM Weapons is provided through the application of lossy insulation and active cold plasma manipulation within the cavity between the aircraft graphite unibody and aramid external skins.
--
Anti-LIDAR COMPOSITE(Implemented by Finland)
How it functions: A thin layer of composite light-metallic materials is applied to components of an aircraft. THis thin layer of composite material is covered with microscopic silica material that is placed to seperate LIDAR rays into opposite adjacent directions.
Specs:
Best Range: 15 km
Additional aircraft weight: over 15 LBS on FA 18C
*details classified*
Counter-Measures.
Radar Warning Receiver
Infra-red Warning Receiver
Active radar jammer
--
For Defense against incoming missiles,Micronesia has implemented the MAAMG or Advanced Aerial Air-To-Air Guns.These guns are designed to engage incoming Air-To-Air Missiles.
--
The Su-63 has various systems built in.These systems as developed by the USSR are called "LSS" or Lifetime Support Systems.
Export Price: 110 million USD
MTAAM-3 Silencer Air to Air Missile
Type: MADAAM (Most ADvanced Air to Air Missile)
Propulsion: The Silencer uses a SCRAMjet engine, which instead of using an independent chamber for oxygen it uses oxygen from the atmosphere in order to light the fuel chamber, saving the space which could be used instead to add more fuel, giving the missiles a much longer range. In order to further this range the engine is made of a Ni based superalloy with high Cr content and using the d-electron concept. The d-electron concept was developed on the basis of the molecular orbital calculations of the electronic structures of Ni alloys. The two electronic parameters that are important for this concept are the bond order between an alloying element and nickel atons, Bo, and the other is the d-orbital energy level of alloing elements. This specific composition has high hot-corrossion resistance, tested by the immersion test, where it was tested through weight loss. There is a second coating oa Rene N6 single crystal based superalloy called CMSX-11B and CMSX-116, containing Chromium levels of 12.5% to 14.5% respectively. The Rene N6 also increases hydrogen resistance (HEE).
Sources:
"Rene N6: Third Generation Single Crystal Superalloy", W.S. Walton, K.S. O'Hara, E.E. Ross, T.M. Pollock, and W.H. Murphy. Superalloys 1996
"The Development of the CSMX-11B and CMSX-11C Alloyus for Industrial Gas Turbine Application", G.L. Erickson. Superalloys 1996
"Hot Corrosion Resistant and High Strength Nickel-Based Single Crystal and Directionally-Solidified Superalloys Developed by the d-Electrons Concept", C. Sarioglu, C. Stinner, J.R. Blachere, N. Birks, F.S. Pettit, G.H. Meter, and J.L. Smia
lek. Superalloys 1996
Range: The maximum range is 275 kilometers
Maximum Velocity: Mach 4.7 (decreasing range)
Optimum Velocity: 3.7 for maximum range
Guidance System: The Silencer uses a computer which means it's guided bu the MRT-2 RADAR system on the Hawk and Falcon, and can be programmed to be compatible with any RADAR, including ground RADAR. The missile also has a miniature RADAR with a twenty kilometer range for its terminal phase. The Predator is also programmed for use of surface SODAR and CELLDAR systems if available.
The missile also has a heterodyne-reception optical RADAR using a standard configuration [transmitter laser > exit optics > atmospheric propagation path > target] and [photodetector > photocurrent processing > image processing / BermCombiner/ local oscillato entrance optics]. The Silencer's transmitter is a Casegrainian telescope/ Picture coming soon...
Sources:
"Requirements of a coherent laser pulse-Doppler radar", G. Biernson, R.F. Lucy.
"Analysis and optimization of laser techniques", Graham W. Flint
"Motion sensing by optical heterodyne Doppler detection from diffuse surfaces", R.D. Kroeger
"Optical antenna gain. 1: Transmitting antennas", Bernard J. Klein and Jon J. Degnan
"Optical antenna gain. 2: Recceiving antennas", Bernard J. Klein and Jon J. Degnan
"Imaging and target detection with a heterodyne-reception optical radar", J.H. Shapiro, B.A. Capron, R.C. Harney
Explosion Style: Spread explosion or direct impact. Area of effectiveness is ten kilometers.
Length: 2.1 meters
Diamter: 15 centimeters
Missile Warhead: 20 kilograms Octagen
NO PRODUCTION RIGHTS! It also has one of those handy dandy self-destruction devices every one uses, you know..if you try to copy them.
Costumers with over one million combined purchases have 20% off from new purchases. They are listed below:
Price: 1.1 million USD
Picture coming soon...in drawing phase
SRSB Naram-Sin
(Short Range Strategical Bomber)
Abstract: The Naram-Sin is an extension program to the old Western Asian BMV ULA (came out near September 2003), and an improvement over the BMV/MA-1 ULA Gilgamesh (released November 2004). The new SRSB Naram-Sin would be able to sit over a battlefield and launch a barrage of missiles into invading armies, using the newly designed SkyCat 2000 transport bays, put onto two parallel bomb bays. The mammoth Naram-Sin could reload the ‘clips’ with missiles on hand and be refuled by air, therefore it would stay in combat for an extended period of time.
Engines: Using ‘air-breathing’, rocket based, combined-cycle engines, first developed as a concept by Preston Carter, the Naram-Sin would act as Hypersonic aircraft, of sorts. However, the Naram-Sim would not be as fuel efficient as Carter’s brainchild, yet substantially more fuel efficient than a normal jet engine. Instead, the engines would throttle pushing the Naram-Sin into the upper atmosphere in a near vertical accension, advancing about ten kilometers. As it descents into denser air the Naram-Sin would be pushed up by the increased aerodynamic lift. The engies would fire again, but unlike Carter’s Hypersoar, the engines have the ability to ‘rotate’ through hydraulics and thus pushes the Naram-Sin back up and backwards, so that the Naram-Sin would oscilate back and forth between two points. Any heat which plagues Hypersonic aircraft such as this would be negated as the Naram-Sin would radiate its heat into space, just like the Hypersoar. A 255,000 kilogram Naram-Sin would weigh as much as the heaviest Ariane 4 yet carry 40% more payload.
The engines are constructed of a single crystal Ni-Fe based superalloy called THYMONEL 8. THYMONEL 8 has a high fatigue resistance and this couples with a low hydrogen environment embrittlement (HEE). THYMONEL 8 exibit high termal conductivity and lower Young’s modulus meaning its beneficial for the thermo-mechanical strength. THYMONEL 8 is another RENE N6 based superalloy, and RENE N6 is microstructurally stable, and does not suffer from SR2, a cellular precipitation reaction which happens beneath coatings.
Maximum Velocity (Without loadout): Mach 1.5 (Mach 11 in the upper atmosphere)
Maximum Velocity (Fully Loaded): Mach 1 (Mach 8 in the upper atmosphere; the Hypersoar has a velocity of Mach 10)
Armaments: Using parallel bomb bays the Naram-Sin could place eight ‘clips’ or missile racks per bomb bay, and then stack them in three ‘levels’, meaning each Naram-Sin would have a total of forty-eight ‘clips’, each with twelve ‘slots’, thus a total of five hundred and seventy-six missiles (!). Now, if enough of a stockpile is put into the craft the Naram-Sin could hold and fire a total of two thousand eight hundred and eighty missiles, giving each Naram-Sin (fully loaded) a 2.8 billion dollar value (putting missiles at export price), which although costly, is very effective. ( Which explains why my own airforce only employs one so far.)
The ideal load out:
192 MTAAM-3 Air to Air Missiles
192 MAAM B Cruise Missiles
192 MLAM or MALAS Missiles
However, one could give it a load out which fits a specific mission better. The racks give the possibility of contraction or expansion of the ‘slots’ to fit missiles better – this is done mechanically and through AI if under the ‘re-load phase’ during combat exercises.
Targeting Systems:
MRT-5 on board RADAR with a 100 kilometers range
MST-2 on board SODAR system
MLT-3 o board LIDAR system
The Naram-Sin also uses land based targeting systems, as well as naval targeting systems.
Crew: 60
Export Cost: 350 million (not including missiles) or 3.5 billion (including ideal missile load out)
MLAM-2 Air to Surface Missile
Propulsion: The MLAM-2 uses a conventional Octagen solid rocket fuel booster to propel itself along the surface of the sea, or extremely low in a land terrain scenario. In order to further the range the engine is made of a Ni based superalloy with high Cr content and using the d-electron concept. The d-electron concept was developed on the basis of the molecular orbital calculations of the electronic structures of Ni alloys. The two electronic parameters that are important for this concept are the bond order between an alloying element and nickel atons, Bo, and the other is the d-orbital energy level of alloing elements. This specific composition has high hot-corrossion resistance, tested by the immersion test, where it was tested through weight loss. There is a second coating oa Rene N6 single crystal based superalloy called CMSX-11B and CMSX-116, containing Chromium levels of 12.5% to 14.5% respectively. The Rene N6 also increases hydrogen resistance (HEE).
Range: The maximum range is 200 kilometers
Maximum Velocity: Mach 2.5
Optimum Velocity: 2.1 for maximum range
Guidance System: The Silencer uses a computer which means it's guided by the MRT-2 RADAR system on the Hawk and Falcon, and can be programmed to be compatible with any RADAR, including ground RADAR. The missile also has a miniature RADAR with a twenty kilometer range for its terminal phase. The Predator is also programmed for use of surface SODAR and CELLDAR systems if available.
The missile also has a heterodyne-reception optical RADAR using a standard configuration [transmitter laser > exit optics > atmospheric propagation path > target] and [photodetector > photocurrent processing > image processing / BermCombiner/ local oscillato entrance optics]. The Silencer's transmitter is a Casegrainian telescope
Explosion Style: Direct impact and high explosive.
Length: 3.9 meters
Diamter: 19 centimeters
Missile Warhead: 200 kilograms OctaNitroCubane
Price:1.3 million USD
MALAS-2
Type:Aerial Launched Anti-Shipping Missing[/u]
Engine:The MALAS-2 uses a conventional engine, with a conventional jet turbine, propelling it at a measly Mach 2.1. However, this lower velocity also allows it to maneuver in the face of enemy surface to air missiles, which may be sent to counter the MALAS-2 at longer ranges, allowing the MALAS-2 to most likely surface massive barrages of long range anti-missile SAMs. In addition, the turbine is coated by the THYMONEL 8 superalloy which is used a lot in Macabee missiles to protected against hydrogen embrittlement (HEE), as well as over heating, giving the MALAS-2 an extremely long range (four hundred kilometers; meaning five four seventy total, taking in mind that it drops the torpedo at around 70 kilometers from the enemy fleet). THYMONEL 8 was a NiFe superalloy mixed by the United States military for its jet turbines (NiFe is Nickel Based Iron Formula superalloy).
The MALAS-2 jet turbine propells the missile capsule, which is much like a bouyancy capsule, however, instead is slimmer. At around seventy kilometers distance the MALAS-2 missile capsule, using RADAR and LIDAR to compute distance, as well as sattelite coordination if their are sattelites present, and the missile capsule breaks releasing an MT-3 torpedo into the water. However, this requires the MALAS-2 to slow down to around 120 kilometers per hour. To decrease speed without allowing the enemy a greater time period to shoot it down, the Principe III has a very advanced jamming system, which jams enemy RADAR, giving it ample time to close the distance, break, and drop the MT-3.
The Torpedo: The MT-3 torpedo uses a rocket engine with a NiAl, alumina formula nickel based superalloy, coating to project itself at fifty knots. The engine uses an MHD type propulsion, however using the NiAl construction to ease the rocket projection. It is a sort of underwater ramjet, first developed by the Russians, and then improved by New Empire, and finally in the hands of the The Macabees. The MT-3 is, consequently, extremely silent. The MT-3 also uses a cavitation absorber on the frame and on the screw; this was first developed by the U.S. Navy for destroyers, and shrunk by the Macabees to fit on a torpedo.
It has a 300kg Octagen warhead, with a hull piercing tip, to burn through the titanium double hulls. However, against a titanium frame it would still, most probably, still require two torpedoes to penetrate. The width of the warhead remains 500mm to be able to use it on the existing tubes on the Toledo class SSN and Spanish ASROC weapons on surface ships.
The MT-3 has a rounder form in order to force water pressure to spread equally along the torpedo, meaning that the torpedo could be fired at deeper depths.
The MT-3 is the only “normal” torpedo in Macabee use up to now. It could be classified as MADCAP, according to New Empire’s classification system. The MT-1 and MT-2 are Super Cavitational torpedoes.
Maximum Range: 470 kilometers
Maximum Velocity: Mach 2.1
Length: 4.3 meters
Diameter: 51 centimeters
Cost: 1.1 million USD
Total Sales: 5
Revenue: 33.8245 billion
RULES
1. Do not ask for production rights. If you really, really, want them send me a telegram and make your offer – but beware, I won’t sell them cheap (in the billions).
2. I can do your math, but I would appreciate it if you would do it yourself.
3. All of these designs have those magic sensors which everyone adds if you try to copy them. If you do copy them and use/sell them I will be knocking on your frontdoor.
4. Don’t clog my thread with criticism. Telegram me if you want to say something, or have a problem with something.
DISCOUNTS
25% discount for allies – if you’re on this (http://forums.jolt.co.uk/showthread.php?t=401190) list you’re good. Does not include Naram-Sin.
10% discount for orders over twenty-five billion.
30% discount for regular costumers. These are people on the following list:
Mekugi
----------------------------------
NOTE: 2005 - 2010
MMA-A3 Falcon
It's termed here as the Su-63 because that's the Malatose designation and he wrote it up as the rest of us gave him the information - he as well gave massive input on the actual design.
With the growing Airforces of the world the Macabee and Malatose Governments decided to come together in this joint effort to create a Air Superiority Fighter beyond the rest.This Fighter was designed to win the skies with its advanced Avionic Systems and to develop precision ground strikes against targets.
The Su-63 FireStorm Air Superiority Fighter.[/i]
[b]STATISTICAL DATA:
HEIGHT:
6.3 m
WINGSPAN:
15.2 m
LENGTH:
22.0m
Engines:
2 x SATURN/LYU'KA AL-67 turbo fan engines with thrust-vectoring nozzles providing STOL capabilities, 160 kN static thrust with 250 kN of afterburner.
FUEL CAPACITY:
2,300 US gal (8,706 liters)
MAXIMUM SPEED @ 14,500 meter :
Mach 2.8
CRUISE SPEED (max performance without afterburner):
1805 kph (Mach 1.7)
STALL SPEED:
120 kph
CLIMB RATE:
28,000 meters per minute
CEILING:
20,000 meters (65 kft)
MIN LANDING DISTANCE AT SEA LEVEL:
300 meters
MAX COMBAT RADIUS:
2500 km
MAX RANGE (without external stores):
5600km
ESTIMATED COST:
$195,000,000
---------
Weapons Systems
2 x One GSh-30-1 30mm: Two GSh-30-1 30-mm cannons are mounted in blisters on either side of the main fuselage. The cannons are mounted on a geared rotor that is driven by a 20-hp electric motor which turns the barrels while each one fires individually. The cannon is capable of firing up to 7,200 rounds per minute with a muzzle velocity of 1,030 meters per second. Each cannon is fed from an internal 800 round storage drum which feeds the cannon with a double-ended hydraulically driven linkless feed system.
13 x BODY/WING HARD POINTS: 25,000 lb (11,340 kg) of external stores can be mounted on six hard points mounted on either wing and four under the main fuselage.
2 Internal Hardpoints: Internal Hardpoints can carry over 2,000lb of Internal Stores,such as bombs or 2 Missiles.
Cockpit
http://img18.exs.cx/img18/6537/cockpit0016ox.gif
The Cockpit of the Su-63 is all glass.There are no traditional round dial, standby or dedicated gauges and the Cockpit is fully Night Vision Compatible.
The GEC-built Head-Up Display (HUD) offers a wide field of view (30 degrees horizontally by 25 degrees vertically) and serves as a primary flight instrument for the pilot.
There are six liquid crystal display (LCD) panels in the cockpit. These present information in full color and are fully readable in direct sunlight. LCDs offer lower weight and less size than the cathode ray tube (CRT) displays used in most current aircraft. The lower power requirements also provide a reliability improvement over CRTs. The two Up-Front Displays (UFDs) measure 3"x4" in size and are located to the left and right of the ICP
The Integrated Control Panel (ICP) is the primary means for manual pilot data entry for communications, navigation, and autopilot data. Located under the glareshield and HUD in center top of the instrument panel, this keypad entry system also has some double click functions, much like a computer mouse for rapid pilot access/use.
The Primary Multi-Function Display (PMFD) is a 8"x8" color display that is located in the middle of the instrument panel, under the ICP. It is the pilot’s principal display for aircraft navigation (including showing waypoints and route of flight) and Situation Assessment (SA) or a "God's-eye view" of the entire environment around (above, below, both sides, front and back) the aircraft.
Three Secondary Multi-Function Displays (SMFDs) are all 6.25" x 6.25" and two of them are located on either side of the PMFD on the instrument panel with the third underneath the PMFD between the pilot's knees. These are used for displaying tactical (both offensive and defensive) information as well as non-tactical information (such as checklists, subsystem status, engine thrust output, and stores management).
CockPit Electronics
2 task-switching MFDs
Multi-node radar indication panel
Octo-functional HUD synchronized with MFD and helmet targeting
GPS synchronization panel
Topographic orientation TRV systems
Autopilot TRV/NRT based systems
JTIDs/A50 airbourne intelligence/global targetting, guidance systems.
APEX 345 ejection seat, syncronized with primary turbine faliures.
LIDAR/RADAR incoming signal indicator/interceptor to JTIDs.
--
Maneuvering System
The Sukhoi Su-63 is an extremely maneuverable fighter using 3D thrust vectoring and an innovated reverse canard design.The Su-63 uses an extensive fly-by-wire system which gives the pilot unprecedented abilities in piloting the aircraft.
Avionics.
The Su-63 uses advanced integrated Avionic Systems developed jointly by Finnish and Soviet Scientist.These systems computing power are equal to that of 7 Cray Super Computers.
--
ACTIVE SENSOR JAMMER: Internal ECM providing broadband RF protection.
AUTO-PILOT: The Su-63 is equipped with a computerized auto-pilot, allowing the pilot to relax or even sleep during long voyages. The auto- pilot can be programmed with a single destination or a complex flight plan involving multiple speeds, directions, and destinations. The onboard computer will alert the pilot when the fighter is near its destination.
OPTICS (NIGHTVISION):100km range. A passive light image intensifier that emits no light of its own, but relies on ambient light which is electronically amplified to produce a visible picture.
NO-12M: Multi-mode X-band pulse Doppler radar. Detection Range is 250km. System consists of a single electronically-scanned Phased-Array RADAR antenna mounted in the nose and tail giving the Su-63 360 degree scanning capabilites.System can track 50 Targets and simultaeneously fire at 5.The NO-12M RADAR can also be integrated with AWAC or ground based RADAR systems to give it a total detection range of 700km.
NO-15M Infra-Red Sensor System: Scans for enemy heat signatures at a range of up to 110km.
NLTS Laser Targeting system: Has a range of 50 km and is used to increase the accuracy of onboard weapons.
NOLDR(LIDAR system): The NOLDR is a heterodyne-reception optical radar system which uses pulse-tone waveforms.The system also uses Doppler RADAR.It reduces backscattering and extinction of coefficient of the atmosphere.
NO-Z2M Intra-Data Link System: Allows for all Su-63 Fighterstorm Fighters to share information automatically without radio calls.The wing leader can also easily glance at the computer and tell how much fuel and weapons his wingmen have left.He can also see which enemy fighter his wingman has targeted.This system allows for the wing commander to assign targets to each of his wingmen also.
RADIO/VIDEO COMMUNICATION: Long range, directional communications system with satellite relay capabilities. Range: 600 miles (960 km) or can be boosted indefinitely via satellite relay.
TACTICAL LIFE SUPPORT SYSTEM: The Su-63 pressurized and provides full nuclear and chemical protection.
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Stealth Technology
The Su-63 employs technologies to significantly reduce Radar Cross Section (RCS), infrared signature, electromagnetic signature, visual signature and aural signature. RCS reduction represents the paramount LO feature considered in the Su-63 design. To reduce RCS, the
S-63 employs a geometrically based radar disbursing configuration. Developed utilizing computational RCS modeling techniques employed and/or developed by Sukhoi, the Su-63 configuration employs facets approximated by curvelinear, polynomial sections. Ultimate Su-63 RCS reduction, however, is dependent upon a proprietary combination of bandpass external skins, internal shaping and the implimentation of Cold-Plasma-Cavity Active Stealth Technology. Between the external bandpass skins and the internal graphite hull backed by an alloy geodetic structure is a cavity. Within this cavity a low temperature plasma is achieved. This plasma, as manipulated actively by the aircraft’s computer driven self-protection network, provides an unparalleled level of active stealth technology whereby incoming interrogative radar energy is substantially disrupted such that return signal is mitigated to undetectable levels or chaotic, undeciferable signals. Rather than rely solely upon external shaping, Sukhoi proprietary Su-63 stealth technology adapts to frequency and bandwidth, allowing maximum LO performance against all air-to-air and ground based radar types alike. Su-63 clean, all-aspect RCS is on the order of 0.006 square meters.
To reduce RCS while carrying external stores, the aircraft can be equipped with Radar Elusive Tactical Stores Dispensers (RETSD™), developed by Sukhoi. These dispensers allow the Su-63 to carry wing mounted external stores without compromising LO features. This allows the Su-63 to conduct precision strike and air-to-air engagements with limited detectability. The Su-63 also features two independent, internal weapons bays for compact internal stores carriage including both the tube-launched short range AAM as well as 250 LB class precision guided munitions. Carriage of compact stores within these internal weapons bays permits a slightly armed Su-63 to function in a "clean" RCS configuration.
Reduction of IR emissions is achieved through the use of a dedicated engine bay cooling/IR signature reduction system. Ducting residual inlet air through the Powerplant Signature Reduction Shroud (PSRS), significantly reduces aircraft IR signature both in the subsonic and supersonic regime. Coupled with Lo-Axi™ or similar LO turbofan exhaust nozzle, the aircraft IR signature is substantially reduced.
Aural signature is reduced in part through the PSRS. For enhanced aural signature reduction, Sukhoi is considering Active Frequency Damping (AFD) and comparable active noise control systems. Visual signature is reduced through employment of smokeless turbofans and by limiting overall aircraft size.
Protection against Scalar EM Weapons is provided through the application of lossy insulation and active cold plasma manipulation within the cavity between the aircraft graphite unibody and aramid external skins.
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Anti-LIDAR COMPOSITE(Implemented by Finland)
How it functions: A thin layer of composite light-metallic materials is applied to components of an aircraft. THis thin layer of composite material is covered with microscopic silica material that is placed to seperate LIDAR rays into opposite adjacent directions.
Specs:
Best Range: 15 km
Additional aircraft weight: over 15 LBS on FA 18C
*details classified*
Counter-Measures.
Radar Warning Receiver
Infra-red Warning Receiver
Active radar jammer
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For Defense against incoming missiles,Micronesia has implemented the MAAMG or Advanced Aerial Air-To-Air Guns.These guns are designed to engage incoming Air-To-Air Missiles.
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The Su-63 has various systems built in.These systems as developed by the USSR are called "LSS" or Lifetime Support Systems.
Export Price: 110 million USD
MTAAM-3 Silencer Air to Air Missile
Type: MADAAM (Most ADvanced Air to Air Missile)
Propulsion: The Silencer uses a SCRAMjet engine, which instead of using an independent chamber for oxygen it uses oxygen from the atmosphere in order to light the fuel chamber, saving the space which could be used instead to add more fuel, giving the missiles a much longer range. In order to further this range the engine is made of a Ni based superalloy with high Cr content and using the d-electron concept. The d-electron concept was developed on the basis of the molecular orbital calculations of the electronic structures of Ni alloys. The two electronic parameters that are important for this concept are the bond order between an alloying element and nickel atons, Bo, and the other is the d-orbital energy level of alloing elements. This specific composition has high hot-corrossion resistance, tested by the immersion test, where it was tested through weight loss. There is a second coating oa Rene N6 single crystal based superalloy called CMSX-11B and CMSX-116, containing Chromium levels of 12.5% to 14.5% respectively. The Rene N6 also increases hydrogen resistance (HEE).
Sources:
"Rene N6: Third Generation Single Crystal Superalloy", W.S. Walton, K.S. O'Hara, E.E. Ross, T.M. Pollock, and W.H. Murphy. Superalloys 1996
"The Development of the CSMX-11B and CMSX-11C Alloyus for Industrial Gas Turbine Application", G.L. Erickson. Superalloys 1996
"Hot Corrosion Resistant and High Strength Nickel-Based Single Crystal and Directionally-Solidified Superalloys Developed by the d-Electrons Concept", C. Sarioglu, C. Stinner, J.R. Blachere, N. Birks, F.S. Pettit, G.H. Meter, and J.L. Smia
lek. Superalloys 1996
Range: The maximum range is 275 kilometers
Maximum Velocity: Mach 4.7 (decreasing range)
Optimum Velocity: 3.7 for maximum range
Guidance System: The Silencer uses a computer which means it's guided bu the MRT-2 RADAR system on the Hawk and Falcon, and can be programmed to be compatible with any RADAR, including ground RADAR. The missile also has a miniature RADAR with a twenty kilometer range for its terminal phase. The Predator is also programmed for use of surface SODAR and CELLDAR systems if available.
The missile also has a heterodyne-reception optical RADAR using a standard configuration [transmitter laser > exit optics > atmospheric propagation path > target] and [photodetector > photocurrent processing > image processing / BermCombiner/ local oscillato entrance optics]. The Silencer's transmitter is a Casegrainian telescope/ Picture coming soon...
Sources:
"Requirements of a coherent laser pulse-Doppler radar", G. Biernson, R.F. Lucy.
"Analysis and optimization of laser techniques", Graham W. Flint
"Motion sensing by optical heterodyne Doppler detection from diffuse surfaces", R.D. Kroeger
"Optical antenna gain. 1: Transmitting antennas", Bernard J. Klein and Jon J. Degnan
"Optical antenna gain. 2: Recceiving antennas", Bernard J. Klein and Jon J. Degnan
"Imaging and target detection with a heterodyne-reception optical radar", J.H. Shapiro, B.A. Capron, R.C. Harney
Explosion Style: Spread explosion or direct impact. Area of effectiveness is ten kilometers.
Length: 2.1 meters
Diamter: 15 centimeters
Missile Warhead: 20 kilograms Octagen
NO PRODUCTION RIGHTS! It also has one of those handy dandy self-destruction devices every one uses, you know..if you try to copy them.
Costumers with over one million combined purchases have 20% off from new purchases. They are listed below:
Price: 1.1 million USD
Picture coming soon...in drawing phase
SRSB Naram-Sin
(Short Range Strategical Bomber)
Abstract: The Naram-Sin is an extension program to the old Western Asian BMV ULA (came out near September 2003), and an improvement over the BMV/MA-1 ULA Gilgamesh (released November 2004). The new SRSB Naram-Sin would be able to sit over a battlefield and launch a barrage of missiles into invading armies, using the newly designed SkyCat 2000 transport bays, put onto two parallel bomb bays. The mammoth Naram-Sin could reload the ‘clips’ with missiles on hand and be refuled by air, therefore it would stay in combat for an extended period of time.
Engines: Using ‘air-breathing’, rocket based, combined-cycle engines, first developed as a concept by Preston Carter, the Naram-Sin would act as Hypersonic aircraft, of sorts. However, the Naram-Sim would not be as fuel efficient as Carter’s brainchild, yet substantially more fuel efficient than a normal jet engine. Instead, the engines would throttle pushing the Naram-Sin into the upper atmosphere in a near vertical accension, advancing about ten kilometers. As it descents into denser air the Naram-Sin would be pushed up by the increased aerodynamic lift. The engies would fire again, but unlike Carter’s Hypersoar, the engines have the ability to ‘rotate’ through hydraulics and thus pushes the Naram-Sin back up and backwards, so that the Naram-Sin would oscilate back and forth between two points. Any heat which plagues Hypersonic aircraft such as this would be negated as the Naram-Sin would radiate its heat into space, just like the Hypersoar. A 255,000 kilogram Naram-Sin would weigh as much as the heaviest Ariane 4 yet carry 40% more payload.
The engines are constructed of a single crystal Ni-Fe based superalloy called THYMONEL 8. THYMONEL 8 has a high fatigue resistance and this couples with a low hydrogen environment embrittlement (HEE). THYMONEL 8 exibit high termal conductivity and lower Young’s modulus meaning its beneficial for the thermo-mechanical strength. THYMONEL 8 is another RENE N6 based superalloy, and RENE N6 is microstructurally stable, and does not suffer from SR2, a cellular precipitation reaction which happens beneath coatings.
Maximum Velocity (Without loadout): Mach 1.5 (Mach 11 in the upper atmosphere)
Maximum Velocity (Fully Loaded): Mach 1 (Mach 8 in the upper atmosphere; the Hypersoar has a velocity of Mach 10)
Armaments: Using parallel bomb bays the Naram-Sin could place eight ‘clips’ or missile racks per bomb bay, and then stack them in three ‘levels’, meaning each Naram-Sin would have a total of forty-eight ‘clips’, each with twelve ‘slots’, thus a total of five hundred and seventy-six missiles (!). Now, if enough of a stockpile is put into the craft the Naram-Sin could hold and fire a total of two thousand eight hundred and eighty missiles, giving each Naram-Sin (fully loaded) a 2.8 billion dollar value (putting missiles at export price), which although costly, is very effective. ( Which explains why my own airforce only employs one so far.)
The ideal load out:
192 MTAAM-3 Air to Air Missiles
192 MAAM B Cruise Missiles
192 MLAM or MALAS Missiles
However, one could give it a load out which fits a specific mission better. The racks give the possibility of contraction or expansion of the ‘slots’ to fit missiles better – this is done mechanically and through AI if under the ‘re-load phase’ during combat exercises.
Targeting Systems:
MRT-5 on board RADAR with a 100 kilometers range
MST-2 on board SODAR system
MLT-3 o board LIDAR system
The Naram-Sin also uses land based targeting systems, as well as naval targeting systems.
Crew: 60
Export Cost: 350 million (not including missiles) or 3.5 billion (including ideal missile load out)
MLAM-2 Air to Surface Missile
Propulsion: The MLAM-2 uses a conventional Octagen solid rocket fuel booster to propel itself along the surface of the sea, or extremely low in a land terrain scenario. In order to further the range the engine is made of a Ni based superalloy with high Cr content and using the d-electron concept. The d-electron concept was developed on the basis of the molecular orbital calculations of the electronic structures of Ni alloys. The two electronic parameters that are important for this concept are the bond order between an alloying element and nickel atons, Bo, and the other is the d-orbital energy level of alloing elements. This specific composition has high hot-corrossion resistance, tested by the immersion test, where it was tested through weight loss. There is a second coating oa Rene N6 single crystal based superalloy called CMSX-11B and CMSX-116, containing Chromium levels of 12.5% to 14.5% respectively. The Rene N6 also increases hydrogen resistance (HEE).
Range: The maximum range is 200 kilometers
Maximum Velocity: Mach 2.5
Optimum Velocity: 2.1 for maximum range
Guidance System: The Silencer uses a computer which means it's guided by the MRT-2 RADAR system on the Hawk and Falcon, and can be programmed to be compatible with any RADAR, including ground RADAR. The missile also has a miniature RADAR with a twenty kilometer range for its terminal phase. The Predator is also programmed for use of surface SODAR and CELLDAR systems if available.
The missile also has a heterodyne-reception optical RADAR using a standard configuration [transmitter laser > exit optics > atmospheric propagation path > target] and [photodetector > photocurrent processing > image processing / BermCombiner/ local oscillato entrance optics]. The Silencer's transmitter is a Casegrainian telescope
Explosion Style: Direct impact and high explosive.
Length: 3.9 meters
Diamter: 19 centimeters
Missile Warhead: 200 kilograms OctaNitroCubane
Price:1.3 million USD
MALAS-2
Type:Aerial Launched Anti-Shipping Missing[/u]
Engine:The MALAS-2 uses a conventional engine, with a conventional jet turbine, propelling it at a measly Mach 2.1. However, this lower velocity also allows it to maneuver in the face of enemy surface to air missiles, which may be sent to counter the MALAS-2 at longer ranges, allowing the MALAS-2 to most likely surface massive barrages of long range anti-missile SAMs. In addition, the turbine is coated by the THYMONEL 8 superalloy which is used a lot in Macabee missiles to protected against hydrogen embrittlement (HEE), as well as over heating, giving the MALAS-2 an extremely long range (four hundred kilometers; meaning five four seventy total, taking in mind that it drops the torpedo at around 70 kilometers from the enemy fleet). THYMONEL 8 was a NiFe superalloy mixed by the United States military for its jet turbines (NiFe is Nickel Based Iron Formula superalloy).
The MALAS-2 jet turbine propells the missile capsule, which is much like a bouyancy capsule, however, instead is slimmer. At around seventy kilometers distance the MALAS-2 missile capsule, using RADAR and LIDAR to compute distance, as well as sattelite coordination if their are sattelites present, and the missile capsule breaks releasing an MT-3 torpedo into the water. However, this requires the MALAS-2 to slow down to around 120 kilometers per hour. To decrease speed without allowing the enemy a greater time period to shoot it down, the Principe III has a very advanced jamming system, which jams enemy RADAR, giving it ample time to close the distance, break, and drop the MT-3.
The Torpedo: The MT-3 torpedo uses a rocket engine with a NiAl, alumina formula nickel based superalloy, coating to project itself at fifty knots. The engine uses an MHD type propulsion, however using the NiAl construction to ease the rocket projection. It is a sort of underwater ramjet, first developed by the Russians, and then improved by New Empire, and finally in the hands of the The Macabees. The MT-3 is, consequently, extremely silent. The MT-3 also uses a cavitation absorber on the frame and on the screw; this was first developed by the U.S. Navy for destroyers, and shrunk by the Macabees to fit on a torpedo.
It has a 300kg Octagen warhead, with a hull piercing tip, to burn through the titanium double hulls. However, against a titanium frame it would still, most probably, still require two torpedoes to penetrate. The width of the warhead remains 500mm to be able to use it on the existing tubes on the Toledo class SSN and Spanish ASROC weapons on surface ships.
The MT-3 has a rounder form in order to force water pressure to spread equally along the torpedo, meaning that the torpedo could be fired at deeper depths.
The MT-3 is the only “normal” torpedo in Macabee use up to now. It could be classified as MADCAP, according to New Empire’s classification system. The MT-1 and MT-2 are Super Cavitational torpedoes.
Maximum Range: 470 kilometers
Maximum Velocity: Mach 2.1
Length: 4.3 meters
Diameter: 51 centimeters
Cost: 1.1 million USD
Total Sales: 5
Revenue: 33.8245 billion