Surperier
22-12-2004, 20:00
The Surperier Market is open to most nations. Some restrictions.
http://fas.org/man/dod-101/sys/ac/f16_1.jpg
F-16
Primary Function Multirole fighter
Builder Lockheed Martin Corp.
Power Plant F-16C/D:
one Pratt and Whitney F100-PW-200/220/229 or
one General Electric F110-GE-100/129
Thrust F-16C/D, 27,000 pounds(12,150 kilograms)
Length 49 feet, 5 inches (14.8 meters)
Height 16 feet (4.8 meters)
Wingspan 32 feet, 8 inches (9.8 meters)
Speed 1,500 mph (Mach 2 at altitude)
Ceiling Above 50,000 feet (15 kilometers)
Maximum Takeoff Weight 37,500 pounds (16,875 kilograms)
Combat Radius [F-16C] 740 nm (1,370 km) w/
2 2,000-lb bombs + 2 AIM-9 + 1,040 US gal external tanks
340 nm (630 km) w/
4 2,000-lb bombs + 2 AIM-9 + 340 US gal external tanks
200 nm (370 km) + 2 hr 10 min patrol
w/ 2 AIM-7 + 2 AIM-9 + 1,040 US gal external tanks
Range Over 2,100 nm (2,425 mi; 3,900 km)
http://fas.org/man/dod-101/sys/ac/f-22_2.jpg
F22
Function Air superiority fighter
Contractors Lockheed Martin Aeronautical Systems: F-22 program management, the integrated forebody (nose section) and forward fuselage (including the cockpit and inlets), leading edges of the wings, the fins and stabilators, flaps, ailerons, landing gear and final assembly of the aircraft.
Lockheed Martin Tactical Aircraft Systems: Center fuselage, stores management, integrated navigation and electronic warfare systems (INEWS), the communications, navigation, and identification (CNI) system, and the weapon support system.
Boeing: wings, aft fuselage (including the structures necessary for engine and nozzle installation), radar system development and testing, avionics integration, the training system, and flight-test development and management.
Pratt & Whitney: F119-PW-100 engines that power the Raptor.
Major Subcontractors (partial list): Northrop Grumman, Texas Instruments, Kidde-Graviner Ltd., Allied-Signal Aerospace, Hughes Radar Systems, Harris, Fairchild Defense, GEC Avionics, Lockheed Sanders, Kaiser Electronics, Digital Equipment Corp., Rosemount Aerospace, Curtiss-Wright Flight Systems, Dowty Decoto, EDO Corp., Lear Astronics Corp., Parker-Hannifin Corp., Simmonds Precision, Sterer Engineering, TRW, XAR, Motorola, Hamilton Standard, Sanders/GE Joint Venture, Menasco Aerospace.
Propulsion two Pratt & Whitney F119-PW-100 engines
Thrust 35,000 lbst
Length 62.08 feet, 18.90 meters
Height 16.67 feet, 5.08 meters
Wingspan 44.5 feet, 13.56 meters
Wing Area 840 square feet
Horizontal Tailspan 29 feet, 8.84 meters
Maximum Takeoff Weight
Ceiling
Speed Mach 1.8 (supercruise: Mach 1.5)
Crew one
Armament Two AIM-9 Sidewinders
six AIM-120C Advanced Medium-Range Air-to-Air Missiles (AMRAAM)
one 20mm Gatling gun
two 1,000-pound Joint Direct Attack Munitions (JDAM)
First flight: September 7, 1997
Date Deployed deliveries beginning in 2002
operational by 2004
http://fas.org/man/dod-101/sys/ac/f-23-ec94-42454-32.jpg
F-23
Contractor Northrop / McDonnell Douglas
Mission Competitor, along with YF-22, in the ATF competition
Length 67 feet, 5 inches (20.6 meters)
Wing span 43 feet, 7 inches (13.3 meters)
Height 13 feet, 11 inches (4.3 meters)
Maximum takeoff weight 64,000 pounds (29,029 kilograms)
Propulsion 2 Pratt and Whitney YF119 turbofan engines, or
2 General Electric YF120 turbofan engines
Speed Mach 2
Range 865-920 miles (750-800 nautical miles) unrefuelled
-Armament 4 AIM-9 Sidewinder - internal bays in engine intake duct sides
4 AIM-120 AMRAAM - internal bays underneath air intakes
Crew One
Unit Cost Unknown
Inventory Two: 1 on display at Western Museum of Flight, in Hawthorne, California
1 on display at USAF Museum USAF Test Center Museum at Edwards Air Force Base, California
http://fas.org/nuke/guide/usa/bomber/b-2_08.jpg
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
16 MK84
36 CBU87
36 CBU89
36 CBU97
PRECISION
8 GBU 27
12 JDAM
8 AGM-154 JSOW
8 AGM-137 TSSAM
Payload: 40,000 pounds (18,000 kilograms)
Crew: Two pilots
Unit cost: Approximately $2.1 billion [average]
Date Deployed: December 1993
Inventory: Active force: 21 (planned operational aircraft); ANG: 0; Reserve: 0
http://fas.org/man/dod-101/sys/land/m1-tank-running-left.jpg
M1A1
Specifications
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
Cruising Range 275 Miles 265 Miles
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
NBC System 200 SCFM - CleanCooled Air
Inventory 403 USMC
Unit Replacement Cost $4,300,000
http://fas.org/man/dod-101/sys/land/m1a1-desert-sand.jpg
M1A2
http://fas.org/man/dod-101/sys/land/m-16-dvic534.jpg
M16A2
Primary function: Infantry weapon
Manufacturer: Colt Manufacturing and Fabrique Nationale Manufacturing Inc.
Length: 39.63 inches (100.66 centimeters)
Weight, with 30 round magazine: 8.79 pounds (3.99 kilograms)
Bore diameter: 5.56mm (.233 inches)
Maximum range :3,600 meters Maximum effective range:
Area target: 2,624.8 feet (800 meters)
Point target: 1,804.5 feet (550 meters)
Muzzle velocity: 2,800 feet (853 meters) per second
Rate of fire:
Cyclic: 800 rounds per minute
Sustained: 12-15 rounds per minute
Semiautomatic: 45 rounds per minute
Burst: 90 rounds per minute
Magazine capacity: 30 rounds
Unit Replacement Cost: $586
http://fas.org/man/dod-101/sys/land/m-249-dvic536.jpg
SAW
Primary function: Hand-held combat machine gun
Manufacturer: Fabrique Nationale Manufacturing, Inc.
Length: 40.87 inches (103.81 centimeters)
Weight:
With bipod and tools: 15.16 pounds (6.88 kilograms)
200-round box magazine: 6.92 pounds (3.14 kilograms)
30-round magazine: 1.07 pounds (.49 kilograms)
Bore diameter: 5.56mm (.233 inches)
Maximum effective range: 3281 feet (1000 meters) for an area target
Maximum range: 2.23 miles (3.6 kilometers)
Rates of fire:
Cyclic: 725 rounds per minute
Sustained: 85 rounds per minute
Unit Replacement Cost: $4,087
More to come soon.
http://fas.org/man/dod-101/sys/ac/f16_1.jpg
F-16
Primary Function Multirole fighter
Builder Lockheed Martin Corp.
Power Plant F-16C/D:
one Pratt and Whitney F100-PW-200/220/229 or
one General Electric F110-GE-100/129
Thrust F-16C/D, 27,000 pounds(12,150 kilograms)
Length 49 feet, 5 inches (14.8 meters)
Height 16 feet (4.8 meters)
Wingspan 32 feet, 8 inches (9.8 meters)
Speed 1,500 mph (Mach 2 at altitude)
Ceiling Above 50,000 feet (15 kilometers)
Maximum Takeoff Weight 37,500 pounds (16,875 kilograms)
Combat Radius [F-16C] 740 nm (1,370 km) w/
2 2,000-lb bombs + 2 AIM-9 + 1,040 US gal external tanks
340 nm (630 km) w/
4 2,000-lb bombs + 2 AIM-9 + 340 US gal external tanks
200 nm (370 km) + 2 hr 10 min patrol
w/ 2 AIM-7 + 2 AIM-9 + 1,040 US gal external tanks
Range Over 2,100 nm (2,425 mi; 3,900 km)
http://fas.org/man/dod-101/sys/ac/f-22_2.jpg
F22
Function Air superiority fighter
Contractors Lockheed Martin Aeronautical Systems: F-22 program management, the integrated forebody (nose section) and forward fuselage (including the cockpit and inlets), leading edges of the wings, the fins and stabilators, flaps, ailerons, landing gear and final assembly of the aircraft.
Lockheed Martin Tactical Aircraft Systems: Center fuselage, stores management, integrated navigation and electronic warfare systems (INEWS), the communications, navigation, and identification (CNI) system, and the weapon support system.
Boeing: wings, aft fuselage (including the structures necessary for engine and nozzle installation), radar system development and testing, avionics integration, the training system, and flight-test development and management.
Pratt & Whitney: F119-PW-100 engines that power the Raptor.
Major Subcontractors (partial list): Northrop Grumman, Texas Instruments, Kidde-Graviner Ltd., Allied-Signal Aerospace, Hughes Radar Systems, Harris, Fairchild Defense, GEC Avionics, Lockheed Sanders, Kaiser Electronics, Digital Equipment Corp., Rosemount Aerospace, Curtiss-Wright Flight Systems, Dowty Decoto, EDO Corp., Lear Astronics Corp., Parker-Hannifin Corp., Simmonds Precision, Sterer Engineering, TRW, XAR, Motorola, Hamilton Standard, Sanders/GE Joint Venture, Menasco Aerospace.
Propulsion two Pratt & Whitney F119-PW-100 engines
Thrust 35,000 lbst
Length 62.08 feet, 18.90 meters
Height 16.67 feet, 5.08 meters
Wingspan 44.5 feet, 13.56 meters
Wing Area 840 square feet
Horizontal Tailspan 29 feet, 8.84 meters
Maximum Takeoff Weight
Ceiling
Speed Mach 1.8 (supercruise: Mach 1.5)
Crew one
Armament Two AIM-9 Sidewinders
six AIM-120C Advanced Medium-Range Air-to-Air Missiles (AMRAAM)
one 20mm Gatling gun
two 1,000-pound Joint Direct Attack Munitions (JDAM)
First flight: September 7, 1997
Date Deployed deliveries beginning in 2002
operational by 2004
http://fas.org/man/dod-101/sys/ac/f-23-ec94-42454-32.jpg
F-23
Contractor Northrop / McDonnell Douglas
Mission Competitor, along with YF-22, in the ATF competition
Length 67 feet, 5 inches (20.6 meters)
Wing span 43 feet, 7 inches (13.3 meters)
Height 13 feet, 11 inches (4.3 meters)
Maximum takeoff weight 64,000 pounds (29,029 kilograms)
Propulsion 2 Pratt and Whitney YF119 turbofan engines, or
2 General Electric YF120 turbofan engines
Speed Mach 2
Range 865-920 miles (750-800 nautical miles) unrefuelled
-Armament 4 AIM-9 Sidewinder - internal bays in engine intake duct sides
4 AIM-120 AMRAAM - internal bays underneath air intakes
Crew One
Unit Cost Unknown
Inventory Two: 1 on display at Western Museum of Flight, in Hawthorne, California
1 on display at USAF Museum USAF Test Center Museum at Edwards Air Force Base, California
http://fas.org/nuke/guide/usa/bomber/b-2_08.jpg
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
16 MK84
36 CBU87
36 CBU89
36 CBU97
PRECISION
8 GBU 27
12 JDAM
8 AGM-154 JSOW
8 AGM-137 TSSAM
Payload: 40,000 pounds (18,000 kilograms)
Crew: Two pilots
Unit cost: Approximately $2.1 billion [average]
Date Deployed: December 1993
Inventory: Active force: 21 (planned operational aircraft); ANG: 0; Reserve: 0
http://fas.org/man/dod-101/sys/land/m1-tank-running-left.jpg
M1A1
Specifications
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
Cruising Range 275 Miles 265 Miles
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
NBC System 200 SCFM - CleanCooled Air
Inventory 403 USMC
Unit Replacement Cost $4,300,000
http://fas.org/man/dod-101/sys/land/m1a1-desert-sand.jpg
M1A2
http://fas.org/man/dod-101/sys/land/m-16-dvic534.jpg
M16A2
Primary function: Infantry weapon
Manufacturer: Colt Manufacturing and Fabrique Nationale Manufacturing Inc.
Length: 39.63 inches (100.66 centimeters)
Weight, with 30 round magazine: 8.79 pounds (3.99 kilograms)
Bore diameter: 5.56mm (.233 inches)
Maximum range :3,600 meters Maximum effective range:
Area target: 2,624.8 feet (800 meters)
Point target: 1,804.5 feet (550 meters)
Muzzle velocity: 2,800 feet (853 meters) per second
Rate of fire:
Cyclic: 800 rounds per minute
Sustained: 12-15 rounds per minute
Semiautomatic: 45 rounds per minute
Burst: 90 rounds per minute
Magazine capacity: 30 rounds
Unit Replacement Cost: $586
http://fas.org/man/dod-101/sys/land/m-249-dvic536.jpg
SAW
Primary function: Hand-held combat machine gun
Manufacturer: Fabrique Nationale Manufacturing, Inc.
Length: 40.87 inches (103.81 centimeters)
Weight:
With bipod and tools: 15.16 pounds (6.88 kilograms)
200-round box magazine: 6.92 pounds (3.14 kilograms)
30-round magazine: 1.07 pounds (.49 kilograms)
Bore diameter: 5.56mm (.233 inches)
Maximum effective range: 3281 feet (1000 meters) for an area target
Maximum range: 2.23 miles (3.6 kilometers)
Rates of fire:
Cyclic: 725 rounds per minute
Sustained: 85 rounds per minute
Unit Replacement Cost: $4,087
More to come soon.