Sony111
14-10-2004, 23:21
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:mp5:RULES OF THE STOREFRONT
:mp5:1. Do your own math
:mp5:2. NO SPAM PLEASE
:mp5:3. This is not a chatroom
:mp5:4. Please state the discount
:mp5:5. If there is something you want but is not in here
please T-gramm me and I shall see that you will
get your order, but at a higher price.
(1-5 million more for shiping and handling)
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Discounts
10% = Purchase of 2-5 billion
15% = Purchase of 5-10 billion
25% = Purchase of 10 or more billion
10% = Allies
5%= If you are in my region
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AIRCRAFTS
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Helacopters
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AH-1 Cobra
Power Plant: Two General Electric T700-GE-401 Turboshaft engines
Each engine delivers 1,690 horsepower.
Accommodations: Two seats, in tandem (pilot in rear, copilot/gunner in front)
Performance: Climb rate: 1,925 feet per minute
Maximum altitude: 14,750 feet
Maximum attainable speed: 170 knots (195 mph)
Maximum cruising speed: 152 knots (173 mph)
Countermeasures: AN/ALE-39 Chaff system and SUU-4/1 Flare dispensers
Armament: One M197 three barrel 20 mm gun (mounted under the nose with 750 round ammo container)
Underwing attachments for four TOW missiles, eight Hellfire missiles, or one AIM-9L Sidewinder missile
Can also be equipped with Zuni rocket launchers
External Dimensions
Main rotor diameter 14.63 m
Main rotor blade chord 00.84 m
Tail rotor diameter 02.97 m
Tail rotor blade chord 00.305 m
Distance between rotor centers 08.89 m
Wing span 03.28 m
Wing aspect ratio 03.74
Length: overall, rotors turning 17.68 m
Length: fuselage 13.87 m
Width overall 03.28 m
Height (to top of rotor head) 04.11 m
Overall height 04.44 m
Ground clearance, main rotor, turning 02.74 m
Elevator span 02.11 m
Width over skids 02.24 m
Areas
Main rotor blades (each) 006.13 m2
Tail rotor blades (each) 000.45 m2
Main rotor disc 168.11 m2
Tail rotor disc 006.94 m2
Vertical fin 002.01 m2
Horizontal tail surfaces 001.41 m2
Weights and Loadings
Weight empty 004.634 kg
Mission fuel load (usable) 946 kg
Maximum useful load (fuel and disposable ordinance) 002.065 kg
Maximum Takeoff and landing weight 006.690 kg
Maximum disc loading 039.80 kg/m2
Maximum power loading 004.42 kg/kW
Performance (At Maximum T-O weight, ISA)
Never exceed speed (Vne) 190 knots
Maximum level speed at S/L 152 knots
Rate of climb at S/L, OEI 244 m/minute
Service ceiling More than 4,720 m
Service ceiling, OEI More than 3,660 m
Hovering ceiling
IGE 4, 495 m
OGE 915 m
Range at S/L with standard fuel, no reserves 317 nm
price= 22 million
AH-64 Apache
Contractors Boeing McDonnell Douglas Helicopter Systems(Mesa, AZ)
General Electric (Lynn, MA)
Martin Marietta (Orlando, FL)
Propulsion Two T700-GE-701Cs
Crew Two
AH-64A AH-64D
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) Lot 1 Weight
Hover In-Ground Effect (MRP) 15,895 ft (4845 m)
[Standard Day]
14,845 ft (4525 m)
[Hot Day ISA + 15C] 14,650 ft (4465 m)
[Standard Day]
13,350 ft (4068 m)
[Hot Day ISA + 15 C]
Hover Out-of-Ground Effect (MRP) 12,685 ft (3866 m)
[Sea Level Standard Day]
11,215 ft (3418 m)
[Hot Day 2000 ft 70 F (21 C)] 10,520 ft (3206 m)
[Standard Day]
9,050 ft (2759 m)
[Hot Day ISA + 15 C]
Vertical Rate of Climb (MRP) 2,175 fpm (663 mpm)
[Sea Level Standard Day]
2,050 fpm (625 mpm)
[Hot Day 2000 ft 70 F (21 C)] 1,775 fpm (541 mpm)
[Sea Level Standard Day]
1,595 fpm (486 mpm)
[Hot Day 2000 ft 70 F (21 C)]
Maximum Rate of Climb (IRP) 2,915 fpm (889 mpm)
[Sea Level Standard Day]
2,890 fpm (881 mpm)
[Hot Day 2000 ft 70 F (21 C)] 2,635 fpm (803 mpm)
[Sea Level Standard Day]
2,600 fpm (793 mpm)
[Hot Day 2000 ft 70 F (21 C)]
Maximum Level Flight Speed 150 kt (279 kph)
[Sea Level Standard Day]
153 kt (284 kph)
[Hot Day 2000 ft 70 F (21 C)] 147 kt (273 kph)
[Sea Level Standard Day]
149 kt (276 kph)
[Hot Day 2000 ft 70 F (21 C)]
Cruise Speed (MCP) 150 kt (279 kph)
[Sea Level Standard Day]
153 kt (284 kph)
[Hot Day 2000 ft 70 F (21 C)] 147 kt (273 kph)
[Sea Level Standard Day]
149 kt (276 kph)
[Hot Day 2000 ft 70 F (21 C)]
Range 400 km - internal fuel
1,900 km - internal and external fuel
Armament M230 30mm 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
Mission Equipment Target Acquisition and Designation System /
Pilot Night Vision System
Reliability The general objective of aircraft readiness is to achieve 75% Mission Capable.
AH-64A Apache Multi-Mission Configurations Primary Mission Starboard Wing M230 Gun Port Wing Rate of Climb Duration
Combat
(Anti-armor) 4 Hellfire 320 rds 30mm 4 Hellfire 1450 fpm 1.8 hours
Multi-role
(Covering force) 4 Hellfire
19 FFAR * 1200 rds 30mm 4 Hellfire
19 FFAR * 860 fpm 2.5 hours
Close-support
(Anti-armor) 8 Hellfire 1200 rds 30mm 8 Hellfire 990 fpm 2.5 hours
Ground-support
(Airmobile escort) 38 FFAR * 1200 rds 30mm 38 FFAR * 780 fpm 2.5 hours
* FFAR = 70mm (2.75 inch) Folding-Fin Aerial Rockets
Price= 30 million
Attackers
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AV-8B Harrier
Contractor: McDonnell Douglas Aircraft (Airframe Prime), Rolls Royce (Engine Prime)
Power Plant: TAV-8B/AV-8B Day Attack (DA): One Rolls Royce Pegasus F402-RR-406 turbofan engine with approximately 20,280 pounds of thrust
AV-8B Night Attack (NA)/AV-8B Radar: One Rolls Royce Pegasus F402-RR-408A turbofan engine with approximately 22,200 pounds of thrust
Accommodations: AV-8B DA/NA/Radar Aircraft: Pilot only
TAV-8B Trainer: Two seats
Performance: Maximum airspeed: 550 KCAS
Range greater than 142 nautical miles high speed/low altitude combat radius
Maximum range: 900 nautical miles
Countermeasures: Not applicable
Armament: One fuselage-mounted 25 mm gun system
Standard Air-to-Ground (A/G) load: Six Mk 82, 500 pound bombs
Standard Air-to-Air (A/A) load: Four AIM-9L/M Sidewinder missiles
Provisions for carrying up to 9,000 pounds of ordnance on seven stations
Mission and Capabilities: The AV-8B single seat Vertical/Short Takeoff and Land (V/STOL) aircraft is the primary close air support/intermediate range intercept/attack mission fixed-wing aircraft for the USMC and the Spanish and Italian navies.
The AV-8B can carry and deliver an assortment of conventional stores such as the Mk 83 1,000 pound GP bomb, GBU-12 500 pound LGB, GBU-16 1,000 LGB, CBU-99/100 Cluster Bomb Units, and 2.75" and 5" rockets.
The NA configuration includes: night vision goggle-compatible cockpit controls and displays, a wide-field-of-view HUD, a Navigation Forward Looking Infrared (NAVFLIR) system, a Digital Map Unit (DMU), and an Angle Rate Bombing System (ARBS) with laser spot tracker, which provides first pass day or night target strike capability at low altitude/high speed.
The Radar aircraft retains all night attack capability but integrates the AN/APG-65 radar system to extend the tracking capabilities of the aircraft for A/G delivery and A/A defense modes.
V/STOL capability allows the AV-8B to be deployed with ground units using amphibious shipping and/or forward basing for rapid close air support response.
Program Summary: All three variants of the AV-8B are in service with the USMC (deployed in WestPac and the Mediterranean).
The Spanish Navy has DA/Radar AV-8Bs.
The Italian Navy has Radar AV-8Bs only.
The U.S., Italy, and Spain are partners in a collaborative international program.
The original DA AV-8B was replaced by the NA variant in 1990, which incorporated the F402-RR-408A engine and expanded night fighting systems such as NAVFLIR, DMU, night vision goggle capability, and wide-field-of-view HUD.
In 1993, the Radar AV-8B was fielded with the full night fighting capability and an AN/APG-65 Radar set to improve A/G and A/A tactical effectiveness.
In 1994, the U.S. began a remanufacturing process to convert DA AV-8Bs to the Radar configuration (REMAN); deliveries began in 1996.
Currently, a NA/Radar AV-8B upgrade program is underway to incorporate an Automatic Target Handoff System (ATHS) and Global Positioning System (GPS) capability into the aircraft.
ATHS allows direct digital target/mission data exchange between the pilot and ground units. GPS integration improves navigational and weapons delivery accuracy.
The AV-8B has seen service in the Persian Gulf (Desert Storm), Somalia (both U.S. and Italian AV-8Bs), and Bosnia (peacekeeping operations).
A total of 51 Radar Aircraft are authorized for procurement by the U.S., Italy, and Spain.
The U.S. has a planned procurement/delivery program for 73 REMAN AV-8Bs (FY 1996 - 2002).
External Dimensions:
Wing Span 9.25 m
Length overall (flying attitude)
AV-8B 14.12 m
TAV-8B 15.32 m
GR. Mks 5/7 14.36 m
T. Mk 10 15.79 m
Height overall 3.55 m
Tailplane span 4.24 m
Outrigger wheel track 5.18 m
Areas
Wings, excl LERX, gross 21.37 m2
LERX (total): Pegasus 11-21 0.81 m2
Pegasus 11-61 1.24 m2
100 percent 1.39 m2
Ailerons (total) 1.15 m2
Trailing-edge flaps (total) 2.88 m2
Ventral fixed strakes (total) 0.51 m2
Ventral retractable fence (LIDs) 0.24 m2
Ventral airbrake 0.42 m2
Fin 2.47 m2
Rudder, excl tab 0.49 m2
Tailplane 4.51 m2
Weights and Loadings (Single-Seaters, Except Where Indicated)
Operating weight empty (including pilot and used fuel)
AV-8B 6,336 kg
GR. Mk 7 7,050 kg
TAV-8B 6,451kg
Maximum fuel
Internal only 3,519 kg
Internal and external 7,180 kg
Maximum external stores
Pegasus 11-61 6,003 kg
Pegasus 11-21/Mk 105* 4,899 kg
Maximum useful load (include fuel, stores, weapons, ammunition and water injection for engine)
Vertical takeoff Approximately 3,062, kg
STO More than 7,710 kg
Basic flight design gross weight for 7g operation 10,410 kg
Maximum T-O weight
435 meters STO 14,061 kg
S/L VTO, ISA:
AV-8B/Pegasus 11-61 9,342 kg
GR. Mk 7 8,700 kg
S/L VTO, 32°C 8,142 kg
Design maximum landing weight 11,340 kg
Maximum vertical landing weight 9,043 kg 205 kg less in TAV-8B
Performance
Maximum mach number in level flight
At S/L 875 knots
At altitude 0.98
STOL takeoff run at maximum takeoff weight:
ISA 435 m
At 32° c 518 m
Operational radius with external loads shown:
Short takeoff (366 m, 12 Mk 82 Snakeye Bombs, internal fuel, 1 hour loiter) 90 nautical miles
Hi-lo-hi, short take off (366 m, seven Mk 82 Snakeye Bombs, two 300 US gallon external fuel tanks no loiter 594 nautical miles
Deck launch intercept mission,
two AIM-9 missiles and two external fuel tanks 627 nautical miles
Unrefueled ferry range
Tanks dropped 1,965 nautical miles
Tanks retained 1,638 nautical miles
Combat air patrol endurance at 100 nautical miles from base. 3 hr.
"G" force limits +8/-3
CHARACTERISTIC
RADAR
NIGHT
ATTACK
DAY
ATTACK
Aircraft Length (feet)
47.75
46.33
46.33
Aircraft Height (feet)
11.66
11.66
11.66
Aircraft Wingspan (feet)
30.35
30.35
30.35
Operating Weight Empty (pounds)
14,912
13,968
13,705
Maximum Vertical Takeoff Weight (pounds)
20,752
20,752
19,185
Maximum Short Takeoff Weight (pounds)
32,000
32,000
31,000
Internal Fuel Weight (pounds)
7,762
7,762
7,762
Maximum External Fuel Weight (pounds)
8,073
8,073
8,073
Price= 25 million
FIGHTERS
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F-14 Tomcat
Function Carrier-based multi-role strike fighter
Contractor Grumman Aerospace Corporation
Propulsion F-14: two Pratt & Whitney TF-30P-414A
turbofan engines with afterburners;
F-14B and F-14D: two General Electric F-110-GE-400
augmented turbofan engines with afterburners
Thrust F-14A: 20,900 pounds (9,405 kg) static thrust per engine;
F-14B and F-14D: 27,000 pounds (12,150 kg) per engine
Length 61 feet 9 inches (18.6 meters)
Height 16 feet (4.8 meters)
Basic Weight approx 43,600 pounds
Maximum Takeoff Weight 72,900 pounds (32,805 kg)
Wingspan 64 feet (19 meters) unswept,
38 feet (11.4 meters) swept
Reference wing area 565 sq ft.
Wing aspect ratio 7.28
Ceiling Above 53,000 feet
Max G 6.5
Speed 1,584 mph (2,548km/h) Max. speed at 40,000 ft (12,200 m)
Max Mach Number = 1.88
Cruise Mach Number = .72
Carrier Approach Speed = 125 kts
Fuel 16, 200 lbs. Internal fuel
3, 800 lbs. External fuel
Maximum range 1,600 nm (2,573km)
Mission Radius 500 nm (930 km) Hi-Med-Hi strike profile
380 nm (700 km) Hi-Lo-Lo-Hi strike profile
Airfield 2,500 ft. Field takeoff distance
2,400 ft. Field landing distance
Crew Two: pilot and radar intercept officer
Armament Up to 13,000 pounds of
Air-to-Air Missiles (up to)
6 AIM-7 Sparrows
4 AIM-9 Sidewinder
6 AIM-54 Phoenix
air-to-ground ordnance
MK-82 (500 lbs.)
4 MK-83 (1,000 lbs.)
4 MK-84 (2,000 lbs.)
MK-20 cluster bomb
4 GBU-10 LGB
GBU-12 MK-82 LGB
4 GBU-16 MK-83 LGB
4 GBU-24 MK-84 LGB
4 GBU-31 JDAM (2,000 lbs)
one MK-61A1 Vulcan 20mm cannon
Selected F-14A and B are wired to carry TARPS
All F-14D's are wired to carry the TARPS
Countermeasures AN/ALR-45 radar warning receiver [Itek]
AN/ALR-67 radar warning receiver [F-14D]
AN/ALQ-167 ECM Pod [F-14D]
AN/ALE-50 towed decoy [F-14D]
Date Deployed First flight: December 21st 1970
Inventory 157 F-14A/B
53 F-14D
Phasing out one squadron / year
All to be withdrawn by 2010
F-14 orginally designed for 6,000 flight hours
Currently certified for 7,350 flight hours
Potential for extension to 8,000 or 9,000 flight hours
Price=40 million
F/A-18 Hornet
Contractor
Boeing [McDonnell Douglas Aerospace] and
Northrop Grumman (Airframe),
General Electric (Engines), and
Hughes (Radar)
F/A-18C/D
Hornet F/A-18E/F
Super Hornet
Power Plant Two F404-GE-402 afterburning engines, each in the 18,000 pound thrust class, which results in a combat thrust-to-weight ratio greater than 1-to-1. Depending on the mission and loading, combat radius is greater than 500 nautical miles. Twin F414-GE-400 engines, each in the 22,000 pound thrust class. On an interdiction mission, the E/F will fly up to 40 % further than the C/D.
Accommodations The F/A-18C and F/A-18E are single seat aircraft.
The D and F models are flown by two crew members.
The aft seat in the D and F may be configured with a stick and throttle for the training environment (or without when crewed with a Weapons System Officer).
Performance F/A-18C maximum speed at level flight in altitudes of 36,089 ft.
Mach 1.7
F/A-18E maximum speed at level flight in altitudes of 36,089 ft.
Mach 1.6
Armament F/A-18C/D can carry up to 13,700 pounds of external ordnance.
Weapon stations include: two wingtip stations for Sidewinders; two outboard wing stations for air-to-air or air-to-ground weapons; two inboard wing stations for fuel tanks, air-to-air, or air-to-ground weapons; two nacelle fuselage stations for AMRAAMs, Sparrows, or sensor pods; and one centerline station for fuel or air-to-ground weapons.
M61 Vulcan 6-barrel rotary cannon with 520 rounds of 20mm ammunition is internally mounted in the nose
AIM-9 Sidewinder
AIM-7F Sparrow
AIM-120 AMRAAM
AGM-65E Maverick
AGM-84 Harpoon
AGM-88A HARM
MK82
10 CBU-87
10 CBU-89
GBU-12
GBU-24
JDAM
B-57 or B-61 Nuclear bomb
F/A-18E/F can carry up to 17,750 pounds of external ordnance; two additional wing store stations have been added.
Mission and Capabilities The F/A-18 Hornet can perform both air-to-air and air-to-ground missions.
Cockpit displays and mission avionics are thoroughly integrated to enhance crew situational awareness and mission capability in high threat, adverse weather/night environments.
Cockpits are night vision goggle compatible.
Multi-Sensor Integration and advanced data link capabilities further enhance situational awareness.
The E/F model will be able to perform a strike tanker mission while carrying a self-protection air-to-air missile loadout.
The E/F model will also have greater payload flexibility, increased mission radius, survivability, payload bring back, and a substantial avionics growth potential.
Price= 20 million
Bombers
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B-1B
Primary Function: Long-range, multi-role, heavy bomber
Builder: 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
Date Deployed: June 1985
Inventory: 100 total production
92 total current inventory
Active force, 51 PMAI (68 actual)
ANG, 18 PMAI (22 actual)
Reserve, 0
AFMC, 2 (Test)
price = 210 million
B-2
Primary function: Multi-role heavy bomber.
Prime Contractor: Northrop Grumman Corp.
Contractor Team: Boeing Military Airplanes Co.,
General Electric Aircraft Engine Group
Hughes Training Inc., Link Division
Power Plant/Manufacturer: Four General Electric F-118-GE-100 engines
Thrust: 17,300 pounds each engine (7,847 kilograms)
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 (15,152 meters)
Takeoff Weight (Typical): 336,500 pounds (152,635 kilograms)
Range: Intercontinental, unrefueled
Armament: NUCLEAR
16 B61
16 B83
16 AGM-129 ACM
16 AGM-131 SRAM 2 CONVENTIONAL
80 MK82 [500lb]
16 MK84 [2000lb]
34-36 CBU87
34-36 CBU89
34-36 CBU97
PRECISION
80 GBU-30 JDAM [500lb]
16 GBU-32 JDAM [2000lb]
8 GBU 27
8 EGBU 28
8 GBU 36
8 GBU 37
8-16 AGM-154 JSOW
8-16 AGM-137 TSSAM
Payload: 40,000 pounds (18,000 kilograms)
Crew: Two pilots
price= $2.1 billion
B-49 Flying Wing
Length 53 ft
Height 15 ft
Wingspan 172 ft
Wing Area 4000 Sq Ft 372 Sq M
Weight 193,938 lbs / 87,953 Kg
Propulsion 8 Allison J35-A-15
Range 3155 miles / 5080 Km
Cruise Speed 419 mph / 674 Km/H / 364 Kt
Max Speed 493 Mph 793.00 Km/H 429 Kt
Ceiling 40700 Feet / 12400 M
price= N/A
Ground Systems
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LAV-150 Commando
Crew 3 (Commander, Gunner, Driver) + 2 troops
Combat Weight V-150 21,800 Lbs. V-150S 24,000 lbs.
Hull length V-150 18ft 8 in ; V150S 20ft 2 in
Width 7ft 5 in
Height 6 ft 6in
Ground Clearance 25.5 in
Main Armament Options for the V-150-150S)
2 7.67mm 800 rounds ready, 3000 in hull
2 12.7mm 400 rounds ready , 1,000 in hull
1 20mm Oerlikon 200 rounds ready 200 in hull
1 25 mm 200 ready, 200 in hull
1 20mm Vulcan 1300 rounds ready
1 30mm
1 12.7mm MG and 40mm Grenade launcher
1 76mm 8 round ready, 31 in hull
1 90mm 8rounds ready 31 in hull
1 81mm morter 62 rounds in hull
TOW missile 7 missile in hull
Sensors and Fire Control none
Armor Cadloy steal plate protects against 7.63mm fire
Powerplant Chrysler 191-hp liquid cooled V-8 gasoline engine, power-to-weight ratio 20:23 hp / metric ton
Spension 4x4 ( all wheels powered, front wheels steering), solid beam asle, semi-elliptical multileaf spring, double hydraulic shock absorbers
Speed 55mph, 3.1mph in water, road range 500 miles, cross country range 400 miles
Obstacle Clearance vertical V-100/500 2ft 0 on V-150S 3 ft 0un amphibipous
price= 30 million
M48 Patton Tank
Dimensions Hull length 21ft, with gun forward 30ft 6 in
Width 11ft 11in
Height 10ft 1 in
Ground Clearance 16 in
Track Width 28 in
Weights: Total 52 tons
107,997 lbs [M48A5]
Hull 20 tons
Turret 18 tons
Engine/Transmission 6 tons
Engine cover 2 tons
Track 2 tons each
Basic load 2 tons
Performance:
Range 258 miles / 463 km
Top speed 40 mph / 48 km/h
Fuel consumption: 1 g/mi road, 2 g/mi offroad
Fording: 1.2 m
Vertical Obstacle: 0 .9 m
Gap Crossing: 2.59 m
Powerplant:
Engine Continental AVDS
1790 cu in 690 horsepower
Transmission Alison CD-850
Armament:
Main gun 90 mm rifled cannon 64 rds
105mm /51 cal M68 rfled gun with 54 rounds [M48A5]
Tank Commander .50 cal M2 HB machine gun 3000 rds
Coax 7.62mm M73 machine gun 10,000 rds
Ammunition: HEAT (High Explosive Anti-Tank)
HEP (High Explosive Plastic)
Canister
WP (White Phosphorus)
Beehive
Armor: Homogeneous cast steel
Hull Front 120 mm
Hull Side, front 76 mm
Hull Side, rear 51 mm
Hull rear 44 mm
Hull floor 25 mm
Turret Front 110 mm
Turret Side 76 mm
Turret Rear 50 mm
Crew: 4 (driver, gunner, loader, TC)
price= 28 million
M1 Abrams Main Battle Tank
M1 / IPM1 M1A1 M1A2
Manufacturer General Dynamics (Land Systems Division)
Crew 4: Commander, Gunner, Loader & Driver
Weight 60 Tons 63 Tons 69.54 Tons
Length (Gun Forward) 384.5 inches 387 inches
Turret Height 93.5 inches
Width 143.8 inches 144 inches
Ground Clearance 19 inches
Ground Pressure 13.1 PSI 13.8 PSI 15.4 PSI
Obstacle Crossing 49 inches 42 inches
Vertical Trench 9 Feet
Power plant AGT-1500 turbine engine
Power Rating 1500 HP
Power to Weight Ratio 25 hp/ton 23.8 hp/ton 21.6 hp/ton
Hydro Kinetic Transmission 4 Speed Forward
2 Speed Reverse
Speed - Maximum 45 mph (Governed) 42 mph (Governed)
Speed - Cross Country 30 mph
Speed - 10% Slope 20 mph 17 mph
Speed - 60% Slope 4.5 mph 4.1 mph
Acceleration
(0 to 20 mph) 7 Seconds 7.2 Seconds
Fuel Capacity 498 gal (1,885 liters) / 505 gal (1,907 liters)
Cruising Range 275 Miles 265 Miles
Fuel Consumption A tank will need approximately 300 gallons every eight hours; this will vary depending on mission, terrain, and weather. A single tank takes 10 minutes to refuel. Refueling and rearming of a tank platoon--four tanks--is approximately 30 minutes under ideal conditions.
0.6 miles per gallon.
60 gallons per hour when traveling cross-country
30+ gallons per hour while operating at a tactical ideal
10 gallons basic idle
A mine plow will increase the fuel consummation rate of a tank by 25 percent
Main Armament 105mm M68A1
Rifled Cannon 120mm M256
Smooth Bore Cannon
Commander's Weapon .50 Cal M2 Machinegun
Coaxial Weapon 7.62 M240 Machinegun
Loader's Weapon 7.62 M240 Machinegun on Skate Mount
Basic Load Main Gun 40 rounds (M1A2 42 rounds)
Commander's 50 Caliber MG 1,000 rounds
M240 7.62 MG (COAX)/Loader's M240 MG 10,800 rounds
Smoke Grenades 24 rounds
NBC System 200 SCFM - CleanCooled Air
Inventory US Army 4,393 586 M1A2
588 M1A2 SEP
Inventory USMC 403
Inventory Other 777 Egypt 315 Saudi Arabia
218 Kuwait
price= 20 million
recovery
~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
M88 Recovery Vehicle
Manufacturer BMY Combat Systems Division United Defense, Ground Systems Division
Anniston Army Depot (ANAD)
Primary function recovery vehicle for main battle tanks Improved recovery vehicle for main battle tanks
Length 352.5in (8.27M)(Boom Stowed) 27.13 feet (8.27 meters)
Width 135in (3.43M) At track 11.25 feet (3.43 meters)
Height 123in (3.13M) Boom Stowed 10.25 feet (3.12 meters)
Ground Clearance 17in (0.43m)
Weight, gross, fully loaded 112,000lbs (50,803KG) 70 tons
Power plant 12 Cylinder Diesel 750 HP at 2400 RPM:
Combined Transmission, Differential Steering & Brake Unit
JP-8 Tuned 1,050 HP Engine
Twin Engine Mounted Hydraulic Coolers
Vehicle Speed 27.0 MPH (42KM/HR) w/o Towed Load
18.0 MPH (29KM/HR) w Towed load
4.5 MPH (7.2KM/HR) w Towed Load up to 10% Grade
30 MPH (maximum)
Fuel capacity 400Gal (1515 Liters) 400 gallons
Fuel Consumption 0.7MPG (9.3KM Liter) at 16 MPH
Cruising range 300 miles
Fording depth
Without kit 56 inches
With kit 102 inches
Grade ascending 60%
Trench crossing 103 inches
Boom capacity 35 tons
Vehicle hoisting capability
Spade up 40,000 LB (4 Part Line W/Lockout) 6 tons
Spade down 50,000 LB (4 Part Line) 35 tons
Boom Lift Height (MAX) At 8FT Reach: 22.5 FT
At 4FT Reach: 25 FT
Line Pull Hoist Winch (4Part Line): 50,000 LB
Main Winch : 90,000 LB
At 4FT Reach: 25 FT
Crew 4 enlisted Commander, Driver, Mechanic
price= 20 million
Transport
~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
XM1108
Weight, combat loaded 40,000 lb. (18,144 kg)
Payload 15,000 lb. (6,804 kg)
Ground pressure, combat loaded 8.63 psi (0.60 kg/cm2)
Personnel capacity 3
Fuel tank capacity 130 gallons (492 liters)
PERFORMANCE
Speed on land 41 mi/h (66 km/h)
Acceleration, 0-20 mph 7.1sec
Acceleration, 0-30 mph 16.7 sec
Cruising range 300 mi (483 km)
Turning radius Pivot to infinite
Slope 60%
Side Slope 40%
Trench crossing 86 in. (218 cm)
Vertical wall climbing 30 in. (76 cm)
Gross horsepower-to-weight ratio 20 hp/ton
ENGINE
Make and model Detroit Diesel 6V53TIA
Displacement 318 in.3 (5.2 liter)
Fuel Diesel
Gross horsepower 400 hp
TRANSMISSION, AUTOMATIC
Make and model Allison X200-4B
Type Hydrokinetic
Steering Hydrostatic
Brake type Multiple wet plate
RUNNING GEAR
Suspension Torsion bar
Road wheels 6 per side, 24 inch diameter (61 cm)
Track type Steel double pin, detachable rubber pad
Number of shoes 75 left, 76 right
Track pitch 6 in. (15.2 cm)
Track width 15 in. (38 cm)
Shock absorbers 4 per side
Wheel travel 15.8 in. (40.2 cm)
ELECTRICAL SYSTEM
Generator
Amperes 200, 300 optional
Volts, dc 28
Batteries 4, type 6TL, 120 amp-hr, 12-volt each
ARMAMENT
M50 MG 2,000 ready rds.
SQUAD WEAPONS
Rifles, M16A2, 5.56mm 3
ARMOR
Hull 5083 Aluminum
Cab 5083 Aluminum
Windows Transparent armor with louver covers
FIRE EXTINGUISHERS
Fixed 5 lb. (2.3 kg) CO2 for engine compartment
Portable 5 lb. (2.3 kg) CO2
Price= 15 million
SHIPS
~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
Battleships
~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
BB-4 Iowa-class
Displacement Design: 11,410 tons
Length Overall Length: 362 ft 5 inches
Waterline Length: 360 ft 0 inches
Beam Waterline Beam: 72 ft 3 inches
Draft Hull Draft:
Design Speed 17.09 knots
Power Plant (160 PSI)
Armament 4 - 12in/35 guns [Main Battery]
8 - 8in/35 guns [Main Battery]
6 - 4in/40 guns [Secondary Battery]
20 - 6pdr guns [Secondary Battery]
4 - 1pdr guns [Secondary Battery]
4 - machine guns [Secondary Battery]
4 - 14in torpedo tubes (above water)
Compliment 36 officers
450 enlisted
486
price= 1 billion
BB-43 Tennessee Class
Displacement Design: 33,190 tons
Length Overall Length: 624 ft inches
Waterline Length: 600 ft inches
Beam Waterline Beam: 97 ft 5 3/4 inches
Draft Hull Draft: 31 ft 0 inches
Design Speed 21.0 knots
Power Plant 8 B&W (280 PSI)
Armament 12 - 14in guns [Main Battery]
22 - 5in guns [Secondary Battery]
4 - 3in guns [Secondary Battery]
0 - pdr guns [Secondary Battery]
0 - 30 cal. machine guns [Secondary Battery]
2 - 21 in torpedo tubes (above water)
Compliment 57 officers
1026 enlisted
1083
price= 1.5 billion (1,500,000,000)
Cruisers
~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
CG-16 Leahy class
Displacement 7,800 tons (full load)
Length 533 feet;
Beam 55 feet
Max Speed 33 knots
Power Plant 4 - 1200 psi boilers; 2 geared turbines
2 shafts 85,000 shaft horsepower
Aircraft None - VERTREP hover areas only
Armament Standard Missiles (ER)
ASROC (from MK 16 box launcher)
8 - Harpoon (from two quad launchers)
6 - MK 46 torpedoes (from 2 triple tube mounts)
2 - 20mm Phalanx CIWS
Combat Systems SPS-48 3D Air Search Radar
SPS-49 Air Search Radar
SPS-10 Surface Search Radar or
SPS-67 Surface Search Radar
SQQ-23 Sonar
1 Mk14 Weapon Direction System
4 Mk76 Missile Fire Control System
1 Mk111 ASW Fire Control System
4 SPG-55 Radars
SLQ-25 NIXIE [Mk 6 FANFARE on CG-17]
SLQ-32 EW system
Complement 455 (27 officer, 428 enlisted)
price= 400 million
CA-3 Brooklyn
Displacement (std) 9215 tons
Displacement (full) 10068 tons
Length 402' 6"
Beam 64' 8"
Draft 24'
Powerplant Seven cylindrical boilers with four vertical triple expansion engines
Horsepower 16000ihp
Screws 2
Speed 20
Armor Belt: 3"
Deck: 2.5" - 6"
C.T.: 8.5"
8" Turrets: 5.5" - 8"
Armament 8 x 8"/35 guns in twin turrets
12 x 5"/40 guns in single casemates
12 x 6pdr guns in single mountings
4 x 1pdr guns in single mountings
5 x 18" torpedo tubes above water
Aircraft none
Complement 581
price= 350 million
Subs
~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
SSBN-726 Ohio-Class FBM Submarines
Builders: General Dynamics Electric Boat Division.
Power Plant: One S8G nuclear reactor
core reloaded every nine years
two geared steam turbines,
one shaft, output of 60,000 hp
Length: 560 feet (170.69 meters)
Beam: 42 feet (10.06 meters)
Displacement: Surfaced: 16,764 tons
Submerged:18,750 tons
Speed: Official: 20+ knots (23+ miles per hour, 36.8 +kph)
Actual: 25 knots submerged speed
Operating Depth: Official: "greater than 800 feet"
Actual: greater than 1,000 feet
Armament: 24 - tubes for Trident I and II,
4 - torpedo tubes with Mk48 Torpedoes
Systems: AN/BQQ-6 passive-only spherical bow and conformal sonar arrays
AN/BQR-19 active short range navigation set
AN/BQS-13 Active sonar
AN/BQS-15 high-frequency short range under-ice sonar set
TB-16B or TB-23 passive towed array
AN/BPS-15A I-Band search and navigation radar
AN/WLR-8(V) radar receiver
MK 98 Digital Missile Fire Control System (FCS) for Trident missiles
MK 118 Torpedo FCS
Crew: 15 Officers, 140 Enlisted
price= 50 million
Amphibious Assault
~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
LHD-1 Wasp class
Power Plant Two boilers (600 PSI), two geared steam turbines,
two shafts, 70,000 shaft horsepower
LHD-8 General Electric [GE] "LM 2500 plus" gas turbine engines
Length 844 feet (253.2 meters)
Beam 106 feet (31.8 meters) at waterline
200 feet w/flight deck elevators extended
Draft 27 feet Maximum (Full Load)
36 feet at the stern [ballasted]
Displacement Approx. 40,500 tons (36,450 metric tons) full load
Speed 20+ knots (23.5+ miles per hour)
Range 9,500 nm @ 20 knots
Fuel 6,200 tons, plus
1,232 tons aircraft fuel
Aircraft (Actual mix depends upon mission)
RECENT DEPLOYMENTS
12 - CH-46 Sea Knight helicopters
4 - CH-53 Sea Stallion helicopters
2 - UH-1N Huey helicopters [3 on 11 MEU WestPac 01-1]
4 - AH-1W SuperCobra attack helicopter
6 - AV-8B Harrier attack planes [none on 11 MEU WestPac 01-1]
OR
12 - CH-46 Sea Knight helicopters
9 - CH-53 Sea Stallion helicopters
4 - UH-1N Huey helicopters
4 - AH-1W SuperCobra attack helicopter
6 - AV-8B Harrier attack planes
OR
12 - CH-46 Sea Knight helicopters
9 - CH-53 Sea Stallion helicopters
6 - AV-8B Harrier attack planes
OR
Assault
42 - CH-46 Sea Knight helicopters
OR
Sea Control
20 - AV-8B Harrier attack planes
6 - ASW helicopters
Landing Craft 2 LCU Landing Craft, Utility or
3 LCAC Landing Craft, Air Cushion or
6 LCM-8 Landing Craft, Mechanized or
40 AAV Amphibious Assault Vehicle [normal] or
61 AAV Amphibious Assault Vehicle [stowed]
Armament 2 - MK29 launchers for NATO Sea Sparrow
3 - MK15 20mm Phalanx CIWS mounts
8 - MK33 .50 cal. machine guns
Combat and Control Systems AN/SLQ-49 Chaff Bouys
AN/SLQ-25 NIXIE Towed Torpedo Countermeasures
SRS-1 Combat D/F
AN/SLQ-32(V)3 Electronic Warfare (EW) system
1 AN/SPS-48 radar
1 AN/SPS-49(V)7 radar
1 AN/SPS-64 radar
1 AN/SPS-67 radar
AN/SYS-2 Detection/Tracking System
1 MK-23 Target Acquisition System (TAS)
1 MK-36 Chaff Launcher
MK-91 Fire control System
Crew 104 officers + 1,004 enlisted Ships Company
1,075 Ships Company crewmembers
1,600-1,894 Marine Detachment embarked troops
price= 100 million
Missles/Bombs/Flares/Mines
~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
Missles
~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
RIM-7 Sea Sparrow
Primary Function Air-to-air and surface-to-air radar-guided missile
Contractors Raytheon Co. and General Dynamics
Power 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
AIM-9 Sidewinder
Primary Function Air-to-air missile
Contractor Naval Weapons Center
Power Plant Hercules and Bermite Mk 36 Mod 71, 8 solid-propellant rocket motor
Thrust Classified
Speed Supersonic Mach 2.5
Range 10 to 18 miles depending on altitude
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
25 lbs high explosive for AIM-9H
20.8 lbs high explosive for AIM-9L/M
Launch Weight 190 pounds (85.5 kilograms)
Guidance System Solid-state, infrared homing system
Introduction Date 1956
Unit Cost $84,000
BGM-109 Tomahawk
Primary Function: Long-range subsonic cruise missile for attacking land targets.
Contractor: Raytheon Co. [ex Hughes Missile Systems Co.] Tucson, Ariz.
Power Plant: Williams International F107-WR-402 cruise turbo-fan engine; solid-fuel booster
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: 8 feet 9 inches (2.67 meters)
Range: Land attack, conventional warhead: 600 nautical miles (690 statute miles, 1104 km)
Speed: Subsonic - about 550 mph (880 km/h)
Guidance System: Inertial and TERCOM
price= 500,000
Smart missles
~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
AGM-65 Maverick
Primary Function: Air-to-surface guided missile
Contractors: Hughes Aircraft Co., Raytheon Co.
Power Plant: Thiokol TX-481 solid-propellant rocket motor
Autopilot Proportional Navigation
Stabilizer Wings/Flippers
Propulsion Boost Sustain
Variant AGM-65A/B AGM-65D AGM-65G AGM-65E AGM-65F
Service Air Force Marine Corps Navy
Launch Weight: 462 lbs
(207.90 kg) 485 lbs
(218.25 kg) 670 lbs
(301.50 kg) 630 lbs
(286 kg) 670 lbs
(301.50 kg)
Diameter: 1 foot (30.48 centimeters)
Wingspan: 2 feet, 4 inches (71.12 centimeters)
Range: 17+ miles (12 nautical miles/27 km)
Speed: 1150 km/h
Guidance System: electro-optical television imaging infrared Laser infrared homing
Warhead: 125 pounds
(56.25 kilograms)
cone shaped 300 pounds
(135 kilograms)
delayed-fuse penetrator, heavyweight 125 pounds
(56.25 kilograms)
cone shaped 300 pounds
(135 kilograms)
delayed-fuse penetrator, heavyweight
Explosive 86 lbs. Comp B 80 lbs. PBX(AF)-108
Fuse Contact FMU-135/B
COSTS Air Force
AGM-65D/G Navy
AGM-65E/F
Aircraft: A-10, F-15E and F-16 F/A-18 F/A-18 and AV-8B
price= 300,000
AGM-136 Tacit Rainbow
Span 5 ft. 2 in.
Length 8 ft. 4 in.
Body diameter 2 ft. 3 in.
Weight 430 lbs.
Armament WDU-30/B 40 lb. blast fragmentation warhead
Engine Williams International F121 turbofan of 70 lbs. thrust
Cruising speed Subsonic
Range air-launched = "More than 50 miles"
ground-launched = 430 kilometer
price= 200,000
Dumb Bombs
~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
CBU-24/B
Weight: 800 lbs.
Length: 93 inches
Diameter: 16 inches
Guidance: None
Control: None
Autopilot: None
Propulsion: None
Warhead: 650
Fuse: MK339 BLU26B Anti-material/Anti-personnel bomblets
Aircraft A7(8), F4, (4-8), F11(8), B52 (8)
price= 90,000 per bomb
Cluster Bombs
~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
CBU-24/B Cluster Bomb
Weight: 800 lbs.
Length: 93 inches
Diameter: 16 inches
Guidance: None
Control: None
Autopilot: None
Propulsion: None
Warhead: 650
Fuse: MK339 BLU26B Anti-material/Anti-personnel bomblets
Aircraft A7(8), F4, (4-8), F11(8), B52 (8)
price= 100,000 per bomb
Chemical
[Mandatory background check]
~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
BLU-80/B Bigeye
Prime Contractor: The Marquardt Company
Weight: 595 pounds
Length: 7 feet, 6 inches
Diameter: 13.25 inches
Wing Span: 1 foot, 5.25 inches
Guidance: None
Control: None
Autopilot: None
Propulsion: None
Warhead: VX Agent Weight: 180 pounds
Fuse:
Aircraft
price= 500,000 per bomb
Penetrators
~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
BLU-113 Penetrator
Mission Offensive counter air, close air support, interdiction
Targets Fixed hard
Class 4,000 lb. Penetrator, Blast/Fragmentation
Service Air Force
Contractor Lockheed (BLU-113/B)
National Forge (BLU-113A/B)
Program status Production
First capability 1991
Weight (lbs.) 4,414
Length (in.) 153 bomb body, 223 overall
Diameter (in.) 14.5 bomb body
Explosive 6471bs. Tritonal
Fuze FMU-143 Series
Stabilizer Air Foil Group (Fins)
Guidance method Laser (man-in-the-loop)
Range Greater than 5 nautical miles
Development cost Development cost is not applicable to this munition.
Quantity 125 plus additional production
Platforms F-15E
F-111F
price= 145,500 per bomb
Mines
~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
MK 60 Encapsulated Torpedo (CAPTOR)
The Mk 60 CAPTOR is the US Navy's only deep water mine. The MK-60 CAPTOR, one of the Navy's primary anti submarine weapons, is actually a deepwater moored torpedo launcher. Mine Mk 60 is a sophisticated anti-submarine warfare (ASW) moored mine which is designed to detect and classify submarines and release a modified Torpedo Mk 46 to acquire and attack submerged targets only. This deep water mine is designed to be laid by aircraft or submarine, and is anchored to the ocean floor. The mine utilizes an influence firing device and is able to classify passing submarines. Its acoustic detection system is designed to seek hostile submarines, ignoring surface craft and friendly submarine acoustic signatures. The weapon lies dormant until a target is detected, at which time the torpedo swims out of its capsule to attack and destroy its target. As in other mines, the Mk 60 incorporates an arming-delay. The MK-60 can be deployed by air, submarine, or surface ship. This weapon was developed by the Mine Division of the Naval Ordnance Laboratory, which is now located at the Naval Surface Warfare Center Dahlgren Division, Coastal Systems Station, Panama City, Florida. Because it can be converted to have some operational capability in littoral waters, a modification to CAPTOR is being considered as one of the options for the Littoral Sea Mine (LSM) program.
Specifications
Primary Function Air and ship-launched lightweight torpedo
Contractor Alliant Techsystems
Power Plant Two-speed, reciprocating external combustion;
Mono-propellant (Otto fuel II) fueled
Length 102.36 in. tube launch configuration (from ship) 145 inches (368 centimeters) - Aircraft / Ship laid
132 inches (335 centimeters) Submarine laid
Diameter 12.75 inches
21 inches (53 centimeters) Aircraft / Ship laid
21 inches (53 centimeters) Submarine laid
Weight 517.65 lbs (warshot configuration)
2370 pounds (1077 kilograms) Air / Ship laid
2056 pounds (935 kilograms) Submarine laid
Range 8,000 yards
Depth Greater than 1,200 ft (365.76 meters)
Officially: "Up to 3000 feet (914 meters)"
Speed Greater than 28 knots (32.2 mph, 51.52 kph)
Detection System Reliable acoustic path (RAP) sound propagation
Guidance System Homing mode - Active or passive/active acoustic homing
Launch/search mode - Snake or circle search
Warhead 98 lbs. of PBXN-103 high explosive (bulk charge)
Type- underwater mine
price= 50,000 per mine
Flares
~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
LUU-2 Candle
Air-deployed LUU-2 high-intensity illumination flare are used to illuminate targets. The LUU-2B Flare has a light output rating of 1.8 x 10(6) candlepower and at 1,000 feet altitude illuminates a circle on the ground of 500 meters at 5 lux. The LUU-2 is housed in a pod or canister and is deployed by ejection. The mechanism has a timer on it that deploys the parachute and ignites the flare candle. The flare candle burns magnesium which burns at high temperature emitting an intense bright white light. The consumption of the aluminum cylinder that contains the flare "candle" may add some orange to the light. The LUU-2 flare enhances a pilot's ability to see targets while using Night Vision Goggles. With the introduction of A-10 Warthog Night Vision capability, such flares are not used as frequently as in the past as they provide too much light for the very sensitive goggles. Flares burn at uneven rates and therefore fluctuate in brightness.
The LUU-2 has a burn time of approximately 5 minutes while suspended from a parachute. The pyrotechnic candle consumes the flare housing, reducing flare weight which in turn slows the rate of fall during the last 2 minutes of burn time. At candle burnout an explosive bolt is fired, releasing one parachute support cable which causes the parachute to collapse. While unburned flares falling from high altitude could be dangerous, burned flares are much less dangerous since they are designed to burn up during the fall (even the aluminum casing is burned).
The LUU-2B/B flare is the latest in a series of illuminating flares introduced by Thiokol for nighttime target illumination and rescue missions. Designated as a multi service flare by United States military forces, the LUU-2B/B incorporates improvements and modifications that further enhance its performance and reliability. The LUU-2B/B has been selected by over 30 foreign countries for aircraft-deployed illumination.
The LUU-2B/B flare is compatible with all standard flare launching systems used on helicopter, cargo, and fighter aircraft. It can be deployed from LAU-74 cargo aircraft launchers, aircraft wing-mounted racks, and the SUU-25, 42, and 44 series launchers. It can also be hand launched from aircraft. Developed to meet stringent U.S. military requirements for operational safety and reliability, the LUU-2B/B uses advanced design and materials concepts derived from aerospace technology. The LUU-2B/B is accepted by the Navy for use on carrier-based aircraft.
Specifications
Weight: 30 lb (13.6 kg)
Length: 36 in. (91.4 cm)
Diameter: 4.87 in. (12.4 cm)
Light Output: 1,800,000 candlepower, 1,600,000 candlepower
Burn Time: 240 sec/300 sec
Descent Rate: 8.3 ft/sec (2.5 m/sec)
User: U.S. Navy/Air Force/International
price= 100,000 (Comes in crates of 200)
:mp5:Ammunition (price per crate):mp5:
~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
M-16
Many in crate= 200,000 bullets
price= 18,000
M-60
many in crate= 200,000 bullets
price= 20,000
M-19
many in crate= 500,000 bullets
price= 21,000
M-21
many in crate= 200,000 bullets
price= 21,000
9mm pistol
many in crate= 600,000 bullets
price= 30,000
7.62mm Pistol
many in crate= 600,000 bullets
price= 31,500
[SONY111 IS RESPONSABLE FOR THE CONTENCE OF THIS ADD]
[Thank you]
:mp5:RULES OF THE STOREFRONT
:mp5:1. Do your own math
:mp5:2. NO SPAM PLEASE
:mp5:3. This is not a chatroom
:mp5:4. Please state the discount
:mp5:5. If there is something you want but is not in here
please T-gramm me and I shall see that you will
get your order, but at a higher price.
(1-5 million more for shiping and handling)
~~~~~~~~~~~~~~~~~~
Discounts
10% = Purchase of 2-5 billion
15% = Purchase of 5-10 billion
25% = Purchase of 10 or more billion
10% = Allies
5%= If you are in my region
~~~~~~~~~~~~~~~~~~
AIRCRAFTS
~~~~~~~~~~~~~~~~~~~~~~~~~~~~
Helacopters
~~~~~~~~~~~~~~~~~~~~~~~~~~~~
AH-1 Cobra
Power Plant: Two General Electric T700-GE-401 Turboshaft engines
Each engine delivers 1,690 horsepower.
Accommodations: Two seats, in tandem (pilot in rear, copilot/gunner in front)
Performance: Climb rate: 1,925 feet per minute
Maximum altitude: 14,750 feet
Maximum attainable speed: 170 knots (195 mph)
Maximum cruising speed: 152 knots (173 mph)
Countermeasures: AN/ALE-39 Chaff system and SUU-4/1 Flare dispensers
Armament: One M197 three barrel 20 mm gun (mounted under the nose with 750 round ammo container)
Underwing attachments for four TOW missiles, eight Hellfire missiles, or one AIM-9L Sidewinder missile
Can also be equipped with Zuni rocket launchers
External Dimensions
Main rotor diameter 14.63 m
Main rotor blade chord 00.84 m
Tail rotor diameter 02.97 m
Tail rotor blade chord 00.305 m
Distance between rotor centers 08.89 m
Wing span 03.28 m
Wing aspect ratio 03.74
Length: overall, rotors turning 17.68 m
Length: fuselage 13.87 m
Width overall 03.28 m
Height (to top of rotor head) 04.11 m
Overall height 04.44 m
Ground clearance, main rotor, turning 02.74 m
Elevator span 02.11 m
Width over skids 02.24 m
Areas
Main rotor blades (each) 006.13 m2
Tail rotor blades (each) 000.45 m2
Main rotor disc 168.11 m2
Tail rotor disc 006.94 m2
Vertical fin 002.01 m2
Horizontal tail surfaces 001.41 m2
Weights and Loadings
Weight empty 004.634 kg
Mission fuel load (usable) 946 kg
Maximum useful load (fuel and disposable ordinance) 002.065 kg
Maximum Takeoff and landing weight 006.690 kg
Maximum disc loading 039.80 kg/m2
Maximum power loading 004.42 kg/kW
Performance (At Maximum T-O weight, ISA)
Never exceed speed (Vne) 190 knots
Maximum level speed at S/L 152 knots
Rate of climb at S/L, OEI 244 m/minute
Service ceiling More than 4,720 m
Service ceiling, OEI More than 3,660 m
Hovering ceiling
IGE 4, 495 m
OGE 915 m
Range at S/L with standard fuel, no reserves 317 nm
price= 22 million
AH-64 Apache
Contractors Boeing McDonnell Douglas Helicopter Systems(Mesa, AZ)
General Electric (Lynn, MA)
Martin Marietta (Orlando, FL)
Propulsion Two T700-GE-701Cs
Crew Two
AH-64A AH-64D
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) Lot 1 Weight
Hover In-Ground Effect (MRP) 15,895 ft (4845 m)
[Standard Day]
14,845 ft (4525 m)
[Hot Day ISA + 15C] 14,650 ft (4465 m)
[Standard Day]
13,350 ft (4068 m)
[Hot Day ISA + 15 C]
Hover Out-of-Ground Effect (MRP) 12,685 ft (3866 m)
[Sea Level Standard Day]
11,215 ft (3418 m)
[Hot Day 2000 ft 70 F (21 C)] 10,520 ft (3206 m)
[Standard Day]
9,050 ft (2759 m)
[Hot Day ISA + 15 C]
Vertical Rate of Climb (MRP) 2,175 fpm (663 mpm)
[Sea Level Standard Day]
2,050 fpm (625 mpm)
[Hot Day 2000 ft 70 F (21 C)] 1,775 fpm (541 mpm)
[Sea Level Standard Day]
1,595 fpm (486 mpm)
[Hot Day 2000 ft 70 F (21 C)]
Maximum Rate of Climb (IRP) 2,915 fpm (889 mpm)
[Sea Level Standard Day]
2,890 fpm (881 mpm)
[Hot Day 2000 ft 70 F (21 C)] 2,635 fpm (803 mpm)
[Sea Level Standard Day]
2,600 fpm (793 mpm)
[Hot Day 2000 ft 70 F (21 C)]
Maximum Level Flight Speed 150 kt (279 kph)
[Sea Level Standard Day]
153 kt (284 kph)
[Hot Day 2000 ft 70 F (21 C)] 147 kt (273 kph)
[Sea Level Standard Day]
149 kt (276 kph)
[Hot Day 2000 ft 70 F (21 C)]
Cruise Speed (MCP) 150 kt (279 kph)
[Sea Level Standard Day]
153 kt (284 kph)
[Hot Day 2000 ft 70 F (21 C)] 147 kt (273 kph)
[Sea Level Standard Day]
149 kt (276 kph)
[Hot Day 2000 ft 70 F (21 C)]
Range 400 km - internal fuel
1,900 km - internal and external fuel
Armament M230 30mm 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
Mission Equipment Target Acquisition and Designation System /
Pilot Night Vision System
Reliability The general objective of aircraft readiness is to achieve 75% Mission Capable.
AH-64A Apache Multi-Mission Configurations Primary Mission Starboard Wing M230 Gun Port Wing Rate of Climb Duration
Combat
(Anti-armor) 4 Hellfire 320 rds 30mm 4 Hellfire 1450 fpm 1.8 hours
Multi-role
(Covering force) 4 Hellfire
19 FFAR * 1200 rds 30mm 4 Hellfire
19 FFAR * 860 fpm 2.5 hours
Close-support
(Anti-armor) 8 Hellfire 1200 rds 30mm 8 Hellfire 990 fpm 2.5 hours
Ground-support
(Airmobile escort) 38 FFAR * 1200 rds 30mm 38 FFAR * 780 fpm 2.5 hours
* FFAR = 70mm (2.75 inch) Folding-Fin Aerial Rockets
Price= 30 million
Attackers
~~~~~~~~~~~~~~~~~~~~~~~~~~~~
AV-8B Harrier
Contractor: McDonnell Douglas Aircraft (Airframe Prime), Rolls Royce (Engine Prime)
Power Plant: TAV-8B/AV-8B Day Attack (DA): One Rolls Royce Pegasus F402-RR-406 turbofan engine with approximately 20,280 pounds of thrust
AV-8B Night Attack (NA)/AV-8B Radar: One Rolls Royce Pegasus F402-RR-408A turbofan engine with approximately 22,200 pounds of thrust
Accommodations: AV-8B DA/NA/Radar Aircraft: Pilot only
TAV-8B Trainer: Two seats
Performance: Maximum airspeed: 550 KCAS
Range greater than 142 nautical miles high speed/low altitude combat radius
Maximum range: 900 nautical miles
Countermeasures: Not applicable
Armament: One fuselage-mounted 25 mm gun system
Standard Air-to-Ground (A/G) load: Six Mk 82, 500 pound bombs
Standard Air-to-Air (A/A) load: Four AIM-9L/M Sidewinder missiles
Provisions for carrying up to 9,000 pounds of ordnance on seven stations
Mission and Capabilities: The AV-8B single seat Vertical/Short Takeoff and Land (V/STOL) aircraft is the primary close air support/intermediate range intercept/attack mission fixed-wing aircraft for the USMC and the Spanish and Italian navies.
The AV-8B can carry and deliver an assortment of conventional stores such as the Mk 83 1,000 pound GP bomb, GBU-12 500 pound LGB, GBU-16 1,000 LGB, CBU-99/100 Cluster Bomb Units, and 2.75" and 5" rockets.
The NA configuration includes: night vision goggle-compatible cockpit controls and displays, a wide-field-of-view HUD, a Navigation Forward Looking Infrared (NAVFLIR) system, a Digital Map Unit (DMU), and an Angle Rate Bombing System (ARBS) with laser spot tracker, which provides first pass day or night target strike capability at low altitude/high speed.
The Radar aircraft retains all night attack capability but integrates the AN/APG-65 radar system to extend the tracking capabilities of the aircraft for A/G delivery and A/A defense modes.
V/STOL capability allows the AV-8B to be deployed with ground units using amphibious shipping and/or forward basing for rapid close air support response.
Program Summary: All three variants of the AV-8B are in service with the USMC (deployed in WestPac and the Mediterranean).
The Spanish Navy has DA/Radar AV-8Bs.
The Italian Navy has Radar AV-8Bs only.
The U.S., Italy, and Spain are partners in a collaborative international program.
The original DA AV-8B was replaced by the NA variant in 1990, which incorporated the F402-RR-408A engine and expanded night fighting systems such as NAVFLIR, DMU, night vision goggle capability, and wide-field-of-view HUD.
In 1993, the Radar AV-8B was fielded with the full night fighting capability and an AN/APG-65 Radar set to improve A/G and A/A tactical effectiveness.
In 1994, the U.S. began a remanufacturing process to convert DA AV-8Bs to the Radar configuration (REMAN); deliveries began in 1996.
Currently, a NA/Radar AV-8B upgrade program is underway to incorporate an Automatic Target Handoff System (ATHS) and Global Positioning System (GPS) capability into the aircraft.
ATHS allows direct digital target/mission data exchange between the pilot and ground units. GPS integration improves navigational and weapons delivery accuracy.
The AV-8B has seen service in the Persian Gulf (Desert Storm), Somalia (both U.S. and Italian AV-8Bs), and Bosnia (peacekeeping operations).
A total of 51 Radar Aircraft are authorized for procurement by the U.S., Italy, and Spain.
The U.S. has a planned procurement/delivery program for 73 REMAN AV-8Bs (FY 1996 - 2002).
External Dimensions:
Wing Span 9.25 m
Length overall (flying attitude)
AV-8B 14.12 m
TAV-8B 15.32 m
GR. Mks 5/7 14.36 m
T. Mk 10 15.79 m
Height overall 3.55 m
Tailplane span 4.24 m
Outrigger wheel track 5.18 m
Areas
Wings, excl LERX, gross 21.37 m2
LERX (total): Pegasus 11-21 0.81 m2
Pegasus 11-61 1.24 m2
100 percent 1.39 m2
Ailerons (total) 1.15 m2
Trailing-edge flaps (total) 2.88 m2
Ventral fixed strakes (total) 0.51 m2
Ventral retractable fence (LIDs) 0.24 m2
Ventral airbrake 0.42 m2
Fin 2.47 m2
Rudder, excl tab 0.49 m2
Tailplane 4.51 m2
Weights and Loadings (Single-Seaters, Except Where Indicated)
Operating weight empty (including pilot and used fuel)
AV-8B 6,336 kg
GR. Mk 7 7,050 kg
TAV-8B 6,451kg
Maximum fuel
Internal only 3,519 kg
Internal and external 7,180 kg
Maximum external stores
Pegasus 11-61 6,003 kg
Pegasus 11-21/Mk 105* 4,899 kg
Maximum useful load (include fuel, stores, weapons, ammunition and water injection for engine)
Vertical takeoff Approximately 3,062, kg
STO More than 7,710 kg
Basic flight design gross weight for 7g operation 10,410 kg
Maximum T-O weight
435 meters STO 14,061 kg
S/L VTO, ISA:
AV-8B/Pegasus 11-61 9,342 kg
GR. Mk 7 8,700 kg
S/L VTO, 32°C 8,142 kg
Design maximum landing weight 11,340 kg
Maximum vertical landing weight 9,043 kg 205 kg less in TAV-8B
Performance
Maximum mach number in level flight
At S/L 875 knots
At altitude 0.98
STOL takeoff run at maximum takeoff weight:
ISA 435 m
At 32° c 518 m
Operational radius with external loads shown:
Short takeoff (366 m, 12 Mk 82 Snakeye Bombs, internal fuel, 1 hour loiter) 90 nautical miles
Hi-lo-hi, short take off (366 m, seven Mk 82 Snakeye Bombs, two 300 US gallon external fuel tanks no loiter 594 nautical miles
Deck launch intercept mission,
two AIM-9 missiles and two external fuel tanks 627 nautical miles
Unrefueled ferry range
Tanks dropped 1,965 nautical miles
Tanks retained 1,638 nautical miles
Combat air patrol endurance at 100 nautical miles from base. 3 hr.
"G" force limits +8/-3
CHARACTERISTIC
RADAR
NIGHT
ATTACK
DAY
ATTACK
Aircraft Length (feet)
47.75
46.33
46.33
Aircraft Height (feet)
11.66
11.66
11.66
Aircraft Wingspan (feet)
30.35
30.35
30.35
Operating Weight Empty (pounds)
14,912
13,968
13,705
Maximum Vertical Takeoff Weight (pounds)
20,752
20,752
19,185
Maximum Short Takeoff Weight (pounds)
32,000
32,000
31,000
Internal Fuel Weight (pounds)
7,762
7,762
7,762
Maximum External Fuel Weight (pounds)
8,073
8,073
8,073
Price= 25 million
FIGHTERS
~~~~~~~~~~~~~~~~~~~~~~~~~~~~
F-14 Tomcat
Function Carrier-based multi-role strike fighter
Contractor Grumman Aerospace Corporation
Propulsion F-14: two Pratt & Whitney TF-30P-414A
turbofan engines with afterburners;
F-14B and F-14D: two General Electric F-110-GE-400
augmented turbofan engines with afterburners
Thrust F-14A: 20,900 pounds (9,405 kg) static thrust per engine;
F-14B and F-14D: 27,000 pounds (12,150 kg) per engine
Length 61 feet 9 inches (18.6 meters)
Height 16 feet (4.8 meters)
Basic Weight approx 43,600 pounds
Maximum Takeoff Weight 72,900 pounds (32,805 kg)
Wingspan 64 feet (19 meters) unswept,
38 feet (11.4 meters) swept
Reference wing area 565 sq ft.
Wing aspect ratio 7.28
Ceiling Above 53,000 feet
Max G 6.5
Speed 1,584 mph (2,548km/h) Max. speed at 40,000 ft (12,200 m)
Max Mach Number = 1.88
Cruise Mach Number = .72
Carrier Approach Speed = 125 kts
Fuel 16, 200 lbs. Internal fuel
3, 800 lbs. External fuel
Maximum range 1,600 nm (2,573km)
Mission Radius 500 nm (930 km) Hi-Med-Hi strike profile
380 nm (700 km) Hi-Lo-Lo-Hi strike profile
Airfield 2,500 ft. Field takeoff distance
2,400 ft. Field landing distance
Crew Two: pilot and radar intercept officer
Armament Up to 13,000 pounds of
Air-to-Air Missiles (up to)
6 AIM-7 Sparrows
4 AIM-9 Sidewinder
6 AIM-54 Phoenix
air-to-ground ordnance
MK-82 (500 lbs.)
4 MK-83 (1,000 lbs.)
4 MK-84 (2,000 lbs.)
MK-20 cluster bomb
4 GBU-10 LGB
GBU-12 MK-82 LGB
4 GBU-16 MK-83 LGB
4 GBU-24 MK-84 LGB
4 GBU-31 JDAM (2,000 lbs)
one MK-61A1 Vulcan 20mm cannon
Selected F-14A and B are wired to carry TARPS
All F-14D's are wired to carry the TARPS
Countermeasures AN/ALR-45 radar warning receiver [Itek]
AN/ALR-67 radar warning receiver [F-14D]
AN/ALQ-167 ECM Pod [F-14D]
AN/ALE-50 towed decoy [F-14D]
Date Deployed First flight: December 21st 1970
Inventory 157 F-14A/B
53 F-14D
Phasing out one squadron / year
All to be withdrawn by 2010
F-14 orginally designed for 6,000 flight hours
Currently certified for 7,350 flight hours
Potential for extension to 8,000 or 9,000 flight hours
Price=40 million
F/A-18 Hornet
Contractor
Boeing [McDonnell Douglas Aerospace] and
Northrop Grumman (Airframe),
General Electric (Engines), and
Hughes (Radar)
F/A-18C/D
Hornet F/A-18E/F
Super Hornet
Power Plant Two F404-GE-402 afterburning engines, each in the 18,000 pound thrust class, which results in a combat thrust-to-weight ratio greater than 1-to-1. Depending on the mission and loading, combat radius is greater than 500 nautical miles. Twin F414-GE-400 engines, each in the 22,000 pound thrust class. On an interdiction mission, the E/F will fly up to 40 % further than the C/D.
Accommodations The F/A-18C and F/A-18E are single seat aircraft.
The D and F models are flown by two crew members.
The aft seat in the D and F may be configured with a stick and throttle for the training environment (or without when crewed with a Weapons System Officer).
Performance F/A-18C maximum speed at level flight in altitudes of 36,089 ft.
Mach 1.7
F/A-18E maximum speed at level flight in altitudes of 36,089 ft.
Mach 1.6
Armament F/A-18C/D can carry up to 13,700 pounds of external ordnance.
Weapon stations include: two wingtip stations for Sidewinders; two outboard wing stations for air-to-air or air-to-ground weapons; two inboard wing stations for fuel tanks, air-to-air, or air-to-ground weapons; two nacelle fuselage stations for AMRAAMs, Sparrows, or sensor pods; and one centerline station for fuel or air-to-ground weapons.
M61 Vulcan 6-barrel rotary cannon with 520 rounds of 20mm ammunition is internally mounted in the nose
AIM-9 Sidewinder
AIM-7F Sparrow
AIM-120 AMRAAM
AGM-65E Maverick
AGM-84 Harpoon
AGM-88A HARM
MK82
10 CBU-87
10 CBU-89
GBU-12
GBU-24
JDAM
B-57 or B-61 Nuclear bomb
F/A-18E/F can carry up to 17,750 pounds of external ordnance; two additional wing store stations have been added.
Mission and Capabilities The F/A-18 Hornet can perform both air-to-air and air-to-ground missions.
Cockpit displays and mission avionics are thoroughly integrated to enhance crew situational awareness and mission capability in high threat, adverse weather/night environments.
Cockpits are night vision goggle compatible.
Multi-Sensor Integration and advanced data link capabilities further enhance situational awareness.
The E/F model will be able to perform a strike tanker mission while carrying a self-protection air-to-air missile loadout.
The E/F model will also have greater payload flexibility, increased mission radius, survivability, payload bring back, and a substantial avionics growth potential.
Price= 20 million
Bombers
~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
B-1B
Primary Function: Long-range, multi-role, heavy bomber
Builder: 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
Date Deployed: June 1985
Inventory: 100 total production
92 total current inventory
Active force, 51 PMAI (68 actual)
ANG, 18 PMAI (22 actual)
Reserve, 0
AFMC, 2 (Test)
price = 210 million
B-2
Primary function: Multi-role heavy bomber.
Prime Contractor: Northrop Grumman Corp.
Contractor Team: Boeing Military Airplanes Co.,
General Electric Aircraft Engine Group
Hughes Training Inc., Link Division
Power Plant/Manufacturer: Four General Electric F-118-GE-100 engines
Thrust: 17,300 pounds each engine (7,847 kilograms)
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 (15,152 meters)
Takeoff Weight (Typical): 336,500 pounds (152,635 kilograms)
Range: Intercontinental, unrefueled
Armament: NUCLEAR
16 B61
16 B83
16 AGM-129 ACM
16 AGM-131 SRAM 2 CONVENTIONAL
80 MK82 [500lb]
16 MK84 [2000lb]
34-36 CBU87
34-36 CBU89
34-36 CBU97
PRECISION
80 GBU-30 JDAM [500lb]
16 GBU-32 JDAM [2000lb]
8 GBU 27
8 EGBU 28
8 GBU 36
8 GBU 37
8-16 AGM-154 JSOW
8-16 AGM-137 TSSAM
Payload: 40,000 pounds (18,000 kilograms)
Crew: Two pilots
price= $2.1 billion
B-49 Flying Wing
Length 53 ft
Height 15 ft
Wingspan 172 ft
Wing Area 4000 Sq Ft 372 Sq M
Weight 193,938 lbs / 87,953 Kg
Propulsion 8 Allison J35-A-15
Range 3155 miles / 5080 Km
Cruise Speed 419 mph / 674 Km/H / 364 Kt
Max Speed 493 Mph 793.00 Km/H 429 Kt
Ceiling 40700 Feet / 12400 M
price= N/A
Ground Systems
~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
LAV-150 Commando
Crew 3 (Commander, Gunner, Driver) + 2 troops
Combat Weight V-150 21,800 Lbs. V-150S 24,000 lbs.
Hull length V-150 18ft 8 in ; V150S 20ft 2 in
Width 7ft 5 in
Height 6 ft 6in
Ground Clearance 25.5 in
Main Armament Options for the V-150-150S)
2 7.67mm 800 rounds ready, 3000 in hull
2 12.7mm 400 rounds ready , 1,000 in hull
1 20mm Oerlikon 200 rounds ready 200 in hull
1 25 mm 200 ready, 200 in hull
1 20mm Vulcan 1300 rounds ready
1 30mm
1 12.7mm MG and 40mm Grenade launcher
1 76mm 8 round ready, 31 in hull
1 90mm 8rounds ready 31 in hull
1 81mm morter 62 rounds in hull
TOW missile 7 missile in hull
Sensors and Fire Control none
Armor Cadloy steal plate protects against 7.63mm fire
Powerplant Chrysler 191-hp liquid cooled V-8 gasoline engine, power-to-weight ratio 20:23 hp / metric ton
Spension 4x4 ( all wheels powered, front wheels steering), solid beam asle, semi-elliptical multileaf spring, double hydraulic shock absorbers
Speed 55mph, 3.1mph in water, road range 500 miles, cross country range 400 miles
Obstacle Clearance vertical V-100/500 2ft 0 on V-150S 3 ft 0un amphibipous
price= 30 million
M48 Patton Tank
Dimensions Hull length 21ft, with gun forward 30ft 6 in
Width 11ft 11in
Height 10ft 1 in
Ground Clearance 16 in
Track Width 28 in
Weights: Total 52 tons
107,997 lbs [M48A5]
Hull 20 tons
Turret 18 tons
Engine/Transmission 6 tons
Engine cover 2 tons
Track 2 tons each
Basic load 2 tons
Performance:
Range 258 miles / 463 km
Top speed 40 mph / 48 km/h
Fuel consumption: 1 g/mi road, 2 g/mi offroad
Fording: 1.2 m
Vertical Obstacle: 0 .9 m
Gap Crossing: 2.59 m
Powerplant:
Engine Continental AVDS
1790 cu in 690 horsepower
Transmission Alison CD-850
Armament:
Main gun 90 mm rifled cannon 64 rds
105mm /51 cal M68 rfled gun with 54 rounds [M48A5]
Tank Commander .50 cal M2 HB machine gun 3000 rds
Coax 7.62mm M73 machine gun 10,000 rds
Ammunition: HEAT (High Explosive Anti-Tank)
HEP (High Explosive Plastic)
Canister
WP (White Phosphorus)
Beehive
Armor: Homogeneous cast steel
Hull Front 120 mm
Hull Side, front 76 mm
Hull Side, rear 51 mm
Hull rear 44 mm
Hull floor 25 mm
Turret Front 110 mm
Turret Side 76 mm
Turret Rear 50 mm
Crew: 4 (driver, gunner, loader, TC)
price= 28 million
M1 Abrams Main Battle Tank
M1 / IPM1 M1A1 M1A2
Manufacturer General Dynamics (Land Systems Division)
Crew 4: Commander, Gunner, Loader & Driver
Weight 60 Tons 63 Tons 69.54 Tons
Length (Gun Forward) 384.5 inches 387 inches
Turret Height 93.5 inches
Width 143.8 inches 144 inches
Ground Clearance 19 inches
Ground Pressure 13.1 PSI 13.8 PSI 15.4 PSI
Obstacle Crossing 49 inches 42 inches
Vertical Trench 9 Feet
Power plant AGT-1500 turbine engine
Power Rating 1500 HP
Power to Weight Ratio 25 hp/ton 23.8 hp/ton 21.6 hp/ton
Hydro Kinetic Transmission 4 Speed Forward
2 Speed Reverse
Speed - Maximum 45 mph (Governed) 42 mph (Governed)
Speed - Cross Country 30 mph
Speed - 10% Slope 20 mph 17 mph
Speed - 60% Slope 4.5 mph 4.1 mph
Acceleration
(0 to 20 mph) 7 Seconds 7.2 Seconds
Fuel Capacity 498 gal (1,885 liters) / 505 gal (1,907 liters)
Cruising Range 275 Miles 265 Miles
Fuel Consumption A tank will need approximately 300 gallons every eight hours; this will vary depending on mission, terrain, and weather. A single tank takes 10 minutes to refuel. Refueling and rearming of a tank platoon--four tanks--is approximately 30 minutes under ideal conditions.
0.6 miles per gallon.
60 gallons per hour when traveling cross-country
30+ gallons per hour while operating at a tactical ideal
10 gallons basic idle
A mine plow will increase the fuel consummation rate of a tank by 25 percent
Main Armament 105mm M68A1
Rifled Cannon 120mm M256
Smooth Bore Cannon
Commander's Weapon .50 Cal M2 Machinegun
Coaxial Weapon 7.62 M240 Machinegun
Loader's Weapon 7.62 M240 Machinegun on Skate Mount
Basic Load Main Gun 40 rounds (M1A2 42 rounds)
Commander's 50 Caliber MG 1,000 rounds
M240 7.62 MG (COAX)/Loader's M240 MG 10,800 rounds
Smoke Grenades 24 rounds
NBC System 200 SCFM - CleanCooled Air
Inventory US Army 4,393 586 M1A2
588 M1A2 SEP
Inventory USMC 403
Inventory Other 777 Egypt 315 Saudi Arabia
218 Kuwait
price= 20 million
recovery
~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
M88 Recovery Vehicle
Manufacturer BMY Combat Systems Division United Defense, Ground Systems Division
Anniston Army Depot (ANAD)
Primary function recovery vehicle for main battle tanks Improved recovery vehicle for main battle tanks
Length 352.5in (8.27M)(Boom Stowed) 27.13 feet (8.27 meters)
Width 135in (3.43M) At track 11.25 feet (3.43 meters)
Height 123in (3.13M) Boom Stowed 10.25 feet (3.12 meters)
Ground Clearance 17in (0.43m)
Weight, gross, fully loaded 112,000lbs (50,803KG) 70 tons
Power plant 12 Cylinder Diesel 750 HP at 2400 RPM:
Combined Transmission, Differential Steering & Brake Unit
JP-8 Tuned 1,050 HP Engine
Twin Engine Mounted Hydraulic Coolers
Vehicle Speed 27.0 MPH (42KM/HR) w/o Towed Load
18.0 MPH (29KM/HR) w Towed load
4.5 MPH (7.2KM/HR) w Towed Load up to 10% Grade
30 MPH (maximum)
Fuel capacity 400Gal (1515 Liters) 400 gallons
Fuel Consumption 0.7MPG (9.3KM Liter) at 16 MPH
Cruising range 300 miles
Fording depth
Without kit 56 inches
With kit 102 inches
Grade ascending 60%
Trench crossing 103 inches
Boom capacity 35 tons
Vehicle hoisting capability
Spade up 40,000 LB (4 Part Line W/Lockout) 6 tons
Spade down 50,000 LB (4 Part Line) 35 tons
Boom Lift Height (MAX) At 8FT Reach: 22.5 FT
At 4FT Reach: 25 FT
Line Pull Hoist Winch (4Part Line): 50,000 LB
Main Winch : 90,000 LB
At 4FT Reach: 25 FT
Crew 4 enlisted Commander, Driver, Mechanic
price= 20 million
Transport
~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
XM1108
Weight, combat loaded 40,000 lb. (18,144 kg)
Payload 15,000 lb. (6,804 kg)
Ground pressure, combat loaded 8.63 psi (0.60 kg/cm2)
Personnel capacity 3
Fuel tank capacity 130 gallons (492 liters)
PERFORMANCE
Speed on land 41 mi/h (66 km/h)
Acceleration, 0-20 mph 7.1sec
Acceleration, 0-30 mph 16.7 sec
Cruising range 300 mi (483 km)
Turning radius Pivot to infinite
Slope 60%
Side Slope 40%
Trench crossing 86 in. (218 cm)
Vertical wall climbing 30 in. (76 cm)
Gross horsepower-to-weight ratio 20 hp/ton
ENGINE
Make and model Detroit Diesel 6V53TIA
Displacement 318 in.3 (5.2 liter)
Fuel Diesel
Gross horsepower 400 hp
TRANSMISSION, AUTOMATIC
Make and model Allison X200-4B
Type Hydrokinetic
Steering Hydrostatic
Brake type Multiple wet plate
RUNNING GEAR
Suspension Torsion bar
Road wheels 6 per side, 24 inch diameter (61 cm)
Track type Steel double pin, detachable rubber pad
Number of shoes 75 left, 76 right
Track pitch 6 in. (15.2 cm)
Track width 15 in. (38 cm)
Shock absorbers 4 per side
Wheel travel 15.8 in. (40.2 cm)
ELECTRICAL SYSTEM
Generator
Amperes 200, 300 optional
Volts, dc 28
Batteries 4, type 6TL, 120 amp-hr, 12-volt each
ARMAMENT
M50 MG 2,000 ready rds.
SQUAD WEAPONS
Rifles, M16A2, 5.56mm 3
ARMOR
Hull 5083 Aluminum
Cab 5083 Aluminum
Windows Transparent armor with louver covers
FIRE EXTINGUISHERS
Fixed 5 lb. (2.3 kg) CO2 for engine compartment
Portable 5 lb. (2.3 kg) CO2
Price= 15 million
SHIPS
~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
Battleships
~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
BB-4 Iowa-class
Displacement Design: 11,410 tons
Length Overall Length: 362 ft 5 inches
Waterline Length: 360 ft 0 inches
Beam Waterline Beam: 72 ft 3 inches
Draft Hull Draft:
Design Speed 17.09 knots
Power Plant (160 PSI)
Armament 4 - 12in/35 guns [Main Battery]
8 - 8in/35 guns [Main Battery]
6 - 4in/40 guns [Secondary Battery]
20 - 6pdr guns [Secondary Battery]
4 - 1pdr guns [Secondary Battery]
4 - machine guns [Secondary Battery]
4 - 14in torpedo tubes (above water)
Compliment 36 officers
450 enlisted
486
price= 1 billion
BB-43 Tennessee Class
Displacement Design: 33,190 tons
Length Overall Length: 624 ft inches
Waterline Length: 600 ft inches
Beam Waterline Beam: 97 ft 5 3/4 inches
Draft Hull Draft: 31 ft 0 inches
Design Speed 21.0 knots
Power Plant 8 B&W (280 PSI)
Armament 12 - 14in guns [Main Battery]
22 - 5in guns [Secondary Battery]
4 - 3in guns [Secondary Battery]
0 - pdr guns [Secondary Battery]
0 - 30 cal. machine guns [Secondary Battery]
2 - 21 in torpedo tubes (above water)
Compliment 57 officers
1026 enlisted
1083
price= 1.5 billion (1,500,000,000)
Cruisers
~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
CG-16 Leahy class
Displacement 7,800 tons (full load)
Length 533 feet;
Beam 55 feet
Max Speed 33 knots
Power Plant 4 - 1200 psi boilers; 2 geared turbines
2 shafts 85,000 shaft horsepower
Aircraft None - VERTREP hover areas only
Armament Standard Missiles (ER)
ASROC (from MK 16 box launcher)
8 - Harpoon (from two quad launchers)
6 - MK 46 torpedoes (from 2 triple tube mounts)
2 - 20mm Phalanx CIWS
Combat Systems SPS-48 3D Air Search Radar
SPS-49 Air Search Radar
SPS-10 Surface Search Radar or
SPS-67 Surface Search Radar
SQQ-23 Sonar
1 Mk14 Weapon Direction System
4 Mk76 Missile Fire Control System
1 Mk111 ASW Fire Control System
4 SPG-55 Radars
SLQ-25 NIXIE [Mk 6 FANFARE on CG-17]
SLQ-32 EW system
Complement 455 (27 officer, 428 enlisted)
price= 400 million
CA-3 Brooklyn
Displacement (std) 9215 tons
Displacement (full) 10068 tons
Length 402' 6"
Beam 64' 8"
Draft 24'
Powerplant Seven cylindrical boilers with four vertical triple expansion engines
Horsepower 16000ihp
Screws 2
Speed 20
Armor Belt: 3"
Deck: 2.5" - 6"
C.T.: 8.5"
8" Turrets: 5.5" - 8"
Armament 8 x 8"/35 guns in twin turrets
12 x 5"/40 guns in single casemates
12 x 6pdr guns in single mountings
4 x 1pdr guns in single mountings
5 x 18" torpedo tubes above water
Aircraft none
Complement 581
price= 350 million
Subs
~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
SSBN-726 Ohio-Class FBM Submarines
Builders: General Dynamics Electric Boat Division.
Power Plant: One S8G nuclear reactor
core reloaded every nine years
two geared steam turbines,
one shaft, output of 60,000 hp
Length: 560 feet (170.69 meters)
Beam: 42 feet (10.06 meters)
Displacement: Surfaced: 16,764 tons
Submerged:18,750 tons
Speed: Official: 20+ knots (23+ miles per hour, 36.8 +kph)
Actual: 25 knots submerged speed
Operating Depth: Official: "greater than 800 feet"
Actual: greater than 1,000 feet
Armament: 24 - tubes for Trident I and II,
4 - torpedo tubes with Mk48 Torpedoes
Systems: AN/BQQ-6 passive-only spherical bow and conformal sonar arrays
AN/BQR-19 active short range navigation set
AN/BQS-13 Active sonar
AN/BQS-15 high-frequency short range under-ice sonar set
TB-16B or TB-23 passive towed array
AN/BPS-15A I-Band search and navigation radar
AN/WLR-8(V) radar receiver
MK 98 Digital Missile Fire Control System (FCS) for Trident missiles
MK 118 Torpedo FCS
Crew: 15 Officers, 140 Enlisted
price= 50 million
Amphibious Assault
~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
LHD-1 Wasp class
Power Plant Two boilers (600 PSI), two geared steam turbines,
two shafts, 70,000 shaft horsepower
LHD-8 General Electric [GE] "LM 2500 plus" gas turbine engines
Length 844 feet (253.2 meters)
Beam 106 feet (31.8 meters) at waterline
200 feet w/flight deck elevators extended
Draft 27 feet Maximum (Full Load)
36 feet at the stern [ballasted]
Displacement Approx. 40,500 tons (36,450 metric tons) full load
Speed 20+ knots (23.5+ miles per hour)
Range 9,500 nm @ 20 knots
Fuel 6,200 tons, plus
1,232 tons aircraft fuel
Aircraft (Actual mix depends upon mission)
RECENT DEPLOYMENTS
12 - CH-46 Sea Knight helicopters
4 - CH-53 Sea Stallion helicopters
2 - UH-1N Huey helicopters [3 on 11 MEU WestPac 01-1]
4 - AH-1W SuperCobra attack helicopter
6 - AV-8B Harrier attack planes [none on 11 MEU WestPac 01-1]
OR
12 - CH-46 Sea Knight helicopters
9 - CH-53 Sea Stallion helicopters
4 - UH-1N Huey helicopters
4 - AH-1W SuperCobra attack helicopter
6 - AV-8B Harrier attack planes
OR
12 - CH-46 Sea Knight helicopters
9 - CH-53 Sea Stallion helicopters
6 - AV-8B Harrier attack planes
OR
Assault
42 - CH-46 Sea Knight helicopters
OR
Sea Control
20 - AV-8B Harrier attack planes
6 - ASW helicopters
Landing Craft 2 LCU Landing Craft, Utility or
3 LCAC Landing Craft, Air Cushion or
6 LCM-8 Landing Craft, Mechanized or
40 AAV Amphibious Assault Vehicle [normal] or
61 AAV Amphibious Assault Vehicle [stowed]
Armament 2 - MK29 launchers for NATO Sea Sparrow
3 - MK15 20mm Phalanx CIWS mounts
8 - MK33 .50 cal. machine guns
Combat and Control Systems AN/SLQ-49 Chaff Bouys
AN/SLQ-25 NIXIE Towed Torpedo Countermeasures
SRS-1 Combat D/F
AN/SLQ-32(V)3 Electronic Warfare (EW) system
1 AN/SPS-48 radar
1 AN/SPS-49(V)7 radar
1 AN/SPS-64 radar
1 AN/SPS-67 radar
AN/SYS-2 Detection/Tracking System
1 MK-23 Target Acquisition System (TAS)
1 MK-36 Chaff Launcher
MK-91 Fire control System
Crew 104 officers + 1,004 enlisted Ships Company
1,075 Ships Company crewmembers
1,600-1,894 Marine Detachment embarked troops
price= 100 million
Missles/Bombs/Flares/Mines
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Missles
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RIM-7 Sea Sparrow
Primary Function Air-to-air and surface-to-air radar-guided missile
Contractors Raytheon Co. and General Dynamics
Power 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
AIM-9 Sidewinder
Primary Function Air-to-air missile
Contractor Naval Weapons Center
Power Plant Hercules and Bermite Mk 36 Mod 71, 8 solid-propellant rocket motor
Thrust Classified
Speed Supersonic Mach 2.5
Range 10 to 18 miles depending on altitude
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
25 lbs high explosive for AIM-9H
20.8 lbs high explosive for AIM-9L/M
Launch Weight 190 pounds (85.5 kilograms)
Guidance System Solid-state, infrared homing system
Introduction Date 1956
Unit Cost $84,000
BGM-109 Tomahawk
Primary Function: Long-range subsonic cruise missile for attacking land targets.
Contractor: Raytheon Co. [ex Hughes Missile Systems Co.] Tucson, Ariz.
Power Plant: Williams International F107-WR-402 cruise turbo-fan engine; solid-fuel booster
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: 8 feet 9 inches (2.67 meters)
Range: Land attack, conventional warhead: 600 nautical miles (690 statute miles, 1104 km)
Speed: Subsonic - about 550 mph (880 km/h)
Guidance System: Inertial and TERCOM
price= 500,000
Smart missles
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AGM-65 Maverick
Primary Function: Air-to-surface guided missile
Contractors: Hughes Aircraft Co., Raytheon Co.
Power Plant: Thiokol TX-481 solid-propellant rocket motor
Autopilot Proportional Navigation
Stabilizer Wings/Flippers
Propulsion Boost Sustain
Variant AGM-65A/B AGM-65D AGM-65G AGM-65E AGM-65F
Service Air Force Marine Corps Navy
Launch Weight: 462 lbs
(207.90 kg) 485 lbs
(218.25 kg) 670 lbs
(301.50 kg) 630 lbs
(286 kg) 670 lbs
(301.50 kg)
Diameter: 1 foot (30.48 centimeters)
Wingspan: 2 feet, 4 inches (71.12 centimeters)
Range: 17+ miles (12 nautical miles/27 km)
Speed: 1150 km/h
Guidance System: electro-optical television imaging infrared Laser infrared homing
Warhead: 125 pounds
(56.25 kilograms)
cone shaped 300 pounds
(135 kilograms)
delayed-fuse penetrator, heavyweight 125 pounds
(56.25 kilograms)
cone shaped 300 pounds
(135 kilograms)
delayed-fuse penetrator, heavyweight
Explosive 86 lbs. Comp B 80 lbs. PBX(AF)-108
Fuse Contact FMU-135/B
COSTS Air Force
AGM-65D/G Navy
AGM-65E/F
Aircraft: A-10, F-15E and F-16 F/A-18 F/A-18 and AV-8B
price= 300,000
AGM-136 Tacit Rainbow
Span 5 ft. 2 in.
Length 8 ft. 4 in.
Body diameter 2 ft. 3 in.
Weight 430 lbs.
Armament WDU-30/B 40 lb. blast fragmentation warhead
Engine Williams International F121 turbofan of 70 lbs. thrust
Cruising speed Subsonic
Range air-launched = "More than 50 miles"
ground-launched = 430 kilometer
price= 200,000
Dumb Bombs
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CBU-24/B
Weight: 800 lbs.
Length: 93 inches
Diameter: 16 inches
Guidance: None
Control: None
Autopilot: None
Propulsion: None
Warhead: 650
Fuse: MK339 BLU26B Anti-material/Anti-personnel bomblets
Aircraft A7(8), F4, (4-8), F11(8), B52 (8)
price= 90,000 per bomb
Cluster Bombs
~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
CBU-24/B Cluster Bomb
Weight: 800 lbs.
Length: 93 inches
Diameter: 16 inches
Guidance: None
Control: None
Autopilot: None
Propulsion: None
Warhead: 650
Fuse: MK339 BLU26B Anti-material/Anti-personnel bomblets
Aircraft A7(8), F4, (4-8), F11(8), B52 (8)
price= 100,000 per bomb
Chemical
[Mandatory background check]
~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
BLU-80/B Bigeye
Prime Contractor: The Marquardt Company
Weight: 595 pounds
Length: 7 feet, 6 inches
Diameter: 13.25 inches
Wing Span: 1 foot, 5.25 inches
Guidance: None
Control: None
Autopilot: None
Propulsion: None
Warhead: VX Agent Weight: 180 pounds
Fuse:
Aircraft
price= 500,000 per bomb
Penetrators
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BLU-113 Penetrator
Mission Offensive counter air, close air support, interdiction
Targets Fixed hard
Class 4,000 lb. Penetrator, Blast/Fragmentation
Service Air Force
Contractor Lockheed (BLU-113/B)
National Forge (BLU-113A/B)
Program status Production
First capability 1991
Weight (lbs.) 4,414
Length (in.) 153 bomb body, 223 overall
Diameter (in.) 14.5 bomb body
Explosive 6471bs. Tritonal
Fuze FMU-143 Series
Stabilizer Air Foil Group (Fins)
Guidance method Laser (man-in-the-loop)
Range Greater than 5 nautical miles
Development cost Development cost is not applicable to this munition.
Quantity 125 plus additional production
Platforms F-15E
F-111F
price= 145,500 per bomb
Mines
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MK 60 Encapsulated Torpedo (CAPTOR)
The Mk 60 CAPTOR is the US Navy's only deep water mine. The MK-60 CAPTOR, one of the Navy's primary anti submarine weapons, is actually a deepwater moored torpedo launcher. Mine Mk 60 is a sophisticated anti-submarine warfare (ASW) moored mine which is designed to detect and classify submarines and release a modified Torpedo Mk 46 to acquire and attack submerged targets only. This deep water mine is designed to be laid by aircraft or submarine, and is anchored to the ocean floor. The mine utilizes an influence firing device and is able to classify passing submarines. Its acoustic detection system is designed to seek hostile submarines, ignoring surface craft and friendly submarine acoustic signatures. The weapon lies dormant until a target is detected, at which time the torpedo swims out of its capsule to attack and destroy its target. As in other mines, the Mk 60 incorporates an arming-delay. The MK-60 can be deployed by air, submarine, or surface ship. This weapon was developed by the Mine Division of the Naval Ordnance Laboratory, which is now located at the Naval Surface Warfare Center Dahlgren Division, Coastal Systems Station, Panama City, Florida. Because it can be converted to have some operational capability in littoral waters, a modification to CAPTOR is being considered as one of the options for the Littoral Sea Mine (LSM) program.
Specifications
Primary Function Air and ship-launched lightweight torpedo
Contractor Alliant Techsystems
Power Plant Two-speed, reciprocating external combustion;
Mono-propellant (Otto fuel II) fueled
Length 102.36 in. tube launch configuration (from ship) 145 inches (368 centimeters) - Aircraft / Ship laid
132 inches (335 centimeters) Submarine laid
Diameter 12.75 inches
21 inches (53 centimeters) Aircraft / Ship laid
21 inches (53 centimeters) Submarine laid
Weight 517.65 lbs (warshot configuration)
2370 pounds (1077 kilograms) Air / Ship laid
2056 pounds (935 kilograms) Submarine laid
Range 8,000 yards
Depth Greater than 1,200 ft (365.76 meters)
Officially: "Up to 3000 feet (914 meters)"
Speed Greater than 28 knots (32.2 mph, 51.52 kph)
Detection System Reliable acoustic path (RAP) sound propagation
Guidance System Homing mode - Active or passive/active acoustic homing
Launch/search mode - Snake or circle search
Warhead 98 lbs. of PBXN-103 high explosive (bulk charge)
Type- underwater mine
price= 50,000 per mine
Flares
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LUU-2 Candle
Air-deployed LUU-2 high-intensity illumination flare are used to illuminate targets. The LUU-2B Flare has a light output rating of 1.8 x 10(6) candlepower and at 1,000 feet altitude illuminates a circle on the ground of 500 meters at 5 lux. The LUU-2 is housed in a pod or canister and is deployed by ejection. The mechanism has a timer on it that deploys the parachute and ignites the flare candle. The flare candle burns magnesium which burns at high temperature emitting an intense bright white light. The consumption of the aluminum cylinder that contains the flare "candle" may add some orange to the light. The LUU-2 flare enhances a pilot's ability to see targets while using Night Vision Goggles. With the introduction of A-10 Warthog Night Vision capability, such flares are not used as frequently as in the past as they provide too much light for the very sensitive goggles. Flares burn at uneven rates and therefore fluctuate in brightness.
The LUU-2 has a burn time of approximately 5 minutes while suspended from a parachute. The pyrotechnic candle consumes the flare housing, reducing flare weight which in turn slows the rate of fall during the last 2 minutes of burn time. At candle burnout an explosive bolt is fired, releasing one parachute support cable which causes the parachute to collapse. While unburned flares falling from high altitude could be dangerous, burned flares are much less dangerous since they are designed to burn up during the fall (even the aluminum casing is burned).
The LUU-2B/B flare is the latest in a series of illuminating flares introduced by Thiokol for nighttime target illumination and rescue missions. Designated as a multi service flare by United States military forces, the LUU-2B/B incorporates improvements and modifications that further enhance its performance and reliability. The LUU-2B/B has been selected by over 30 foreign countries for aircraft-deployed illumination.
The LUU-2B/B flare is compatible with all standard flare launching systems used on helicopter, cargo, and fighter aircraft. It can be deployed from LAU-74 cargo aircraft launchers, aircraft wing-mounted racks, and the SUU-25, 42, and 44 series launchers. It can also be hand launched from aircraft. Developed to meet stringent U.S. military requirements for operational safety and reliability, the LUU-2B/B uses advanced design and materials concepts derived from aerospace technology. The LUU-2B/B is accepted by the Navy for use on carrier-based aircraft.
Specifications
Weight: 30 lb (13.6 kg)
Length: 36 in. (91.4 cm)
Diameter: 4.87 in. (12.4 cm)
Light Output: 1,800,000 candlepower, 1,600,000 candlepower
Burn Time: 240 sec/300 sec
Descent Rate: 8.3 ft/sec (2.5 m/sec)
User: U.S. Navy/Air Force/International
price= 100,000 (Comes in crates of 200)
:mp5:Ammunition (price per crate):mp5:
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M-16
Many in crate= 200,000 bullets
price= 18,000
M-60
many in crate= 200,000 bullets
price= 20,000
M-19
many in crate= 500,000 bullets
price= 21,000
M-21
many in crate= 200,000 bullets
price= 21,000
9mm pistol
many in crate= 600,000 bullets
price= 30,000
7.62mm Pistol
many in crate= 600,000 bullets
price= 31,500
[SONY111 IS RESPONSABLE FOR THE CONTENCE OF THIS ADD]
[Thank you]