Post: United States Military (vehicles, Planes, Bombers, Helicopters)(Read and Discuss)
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02-18-2011, 12:47 AM
#1
TheWraith--
Gym leader
//** Note i will update this regulary
**\\ AND BTW THIS IS NOT A USELESS THREAD[multipage=Bombers]
We will start off with the B1-B Lancer:
INFORMATION:
General Characteristics
Primary Function: Long-range, multi-role, heavy bomber
Contractor: Boeing, North America (formerly Rockwell International, North American Aircraft); Offensive avionics, Boeing Military Airplane; defensive avionics, EDO Corporation
Power plant: Four General Electric F101-GE-102 turbofan engine with afterburner
Thrust: 30,000-plus pounds with afterburner, per engine
Wingspan: 137 feet (41.8 meters) extended forward, 79 feet (24.1 meters) swept aft
Length: 146 feet (44.5 meters)
Height: 34 feet (10.4 meters)
Weight: approximately 190,000 pounds (86,183 kilograms)
Maximum Takeoff Weight: 477,000 pounds (216,634 kilograms)
Fuel Capacity: 265,274 pounds (120,326 kilograms)
Payload: 75,000 pounds ( 34,019 kilograms)
Speed: 900-plus mph (Mach 1.2 at sea level)
Range: Intercontinental
Ceiling: More than 30,000 feet (9,144 meters)
Armament: 84 500-pound Mk-82 or 24 2,000-pound Mk-84 general purpose bombs; up to 84 500-pound Mk-62 or 8 2,000-pound Mk-65 Quick Strike naval mines; 30 cluster munitions (CBU-87, -89, -97) or 30 Wind-Corrected Munitions Dispensers (CBU-103, -104, -105); up to 24 2,000-pound GBU-31 or 15 500-pound GBU-38 Joint Direct Attack Munitions; up to 24 AGM-158A Joint Air-to-Surface Standoff Missiles
Crew: Four (aircraft commander, copilot, and two weapon systems officers)
Unit Cost: $283.1 million (fiscal 98 constant dollars)
Initial operating capability: October 1986
Inventory: Active force, 66 (test, 2); ANG, 0; Reserve, 0
Pictures:
[img][IMG]https://i375.photobucket.com/albums/oo194/extender01/chp_b1_lancer.jpg[/img][/IMG]
[img][IMG]https://i118.photobucket.com/albums/o84/NeverEndinJoker/Marines/Rockwell-B-1B-lancer.jpg[/img][/IMG]
B2 Spirit:
INFORMATION:
General Characteristics
Primary function: Multi-role heavy bomber
Contractor: Northrop Grumman Corp. and Contractor Team: Boeing Military Airplanes Co., Hughes Radar Systems Group, General Electric Aircraft Engine Group and Vought Aircraft Industries, Inc.
Power Plant: Four General Electric F118-GE-100 engines
Thrust: 17,300 pounds each engine
Wingspan: 172 feet (52.12 meters)
Length: 69 feet (20.9 meters)
Height: 17 feet (5.1 meters
Weight: 160,000 pounds (72,575 kilograms)
Maximum Takeoff Weight: 336,500 pounds (152,634 kilograms)
Fuel Capacity: 167,000 pounds (75750 kilograms)
Payload: 40,000 pounds (18,144 kilograms)
Speed: High subsonic
Range: Intercontinental
Ceiling: 50,000 feet (15,240 meters)
Armament: Conventional or nuclear weapons
Crew: Two pilots
Unit cost: Approximately $1.157 billion (fiscal 98 constant dollars)
Initial operating capability: April 1997
Inventory: Active force: 20 (1 test); ANG: 0; Reserve: 0
PICTURES:
[img][IMG]https://i126.photobucket.com/albums/p119/zero_cochrane/bombardier-b2-spirit.jpg[/img][/IMG]
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B-52 Stratofortress:
INFORMATION:
General Characteristics
Primary Function: Heavy bomber
Contractor: Boeing Military Airplane Co.
Power plant: Eight Pratt & Whitney engines TF33-P-3/103 turbofan
Thrust: Each engine up to 17,000 pounds
Wingspan: 185 feet (56.4 meters)
Length: 159 feet, 4 inches (48.5 meters)
Height: 40 feet, 8 inches (12.4 meters)
Weight: Approximately 185,000 pounds (83,250 kilograms)
Maximum Takeoff Weight: 488,000 pounds (219,600 kilograms)
Fuel Capacity: 312,197 pounds (141,610 kilograms)
Payload: 70,000 pounds (31,500 kilograms)
Speed: 650 miles per hour (Mach 0.86)
Range: 8,800 miles (7,652 nautical miles)
Ceiling: 50,000 feet (15,151.5 meters)
Armament: Approximately 70,000 pounds (31,500 kilograms) mixed ordnance -- bombs, mines and missiles. (Modified to carry air-launched cruise missiles)
Crew: Five (aircraft commander, pilot, radar navigator, navigator and electronic warfare officer
Unit Cost: $53.4 million (fiscal 98 constant dollars)
Initial operating capability: April 1952
Inventory: Active force, 85; ANG, 0; Reserve, 9
PICTURES:
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C-130 Hercules:
INFORMATION:
General Characteristics
Primary Function: Global airlift
Contractor: Lockheed Martin Aeronautics Company
Power Plant:
C-130E: Four Allison T56-A-7 turboprops; 4,200 prop shaft horsepower
C-130H: Four Allison T56-A-15 turboprops; 4,591prop shaft horsepower
C-130J: Four Rolls-Royce AE 2100D3 turboprops; 4,700 horsepower
Length: C-130E/H/J: 97 feet, 9 inches (29.3 meters)
C-130J-30: 112 feet, 9 inches (34.69 meters)
Height: 38 feet, 10 inches (11. 9 meters)
Wingspan: 132 feet, 7 inches (39.7 meters)
Cargo Compartment:
C-130E/H/J: length, 40 feet (12.31 meters); width, 119 inches (3.12 meters); height, 9 feet (2.74 meters). Rear ramp: length, 123 inches (3.12 meters); width, 119 inches (3.02 meters)
C-130J-30: length, 55 feet (16.9 meters); width, 119 inches (3.12 meters); height, 9 feet (2.74 meters). Rear ramp: length, 123 inches (3.12 meters); width, 119 inches (3.02 meters)
Speed:
C-130E: 345 mph/300 ktas (Mach 0.49) at 20,000 feet (6,060 meters)
C-130H: 366 mph/318 ktas (Mach 0.52) at 20,000 feet (6,060 meters)
C-130J: 417 mph/362 ktas (Mach 0.59) at 22,000 feet (6,706 meters)
C-130J-30: 410 mph/356 ktas (Mach 0.5
at 22,000 feet (6,706 meters)Ceiling:
C-130J: 28,000 feet (8,615 meters) with 42,000 pounds (19,090 kilograms) payload
C-130J-30: 26,000 feet (8,000 meters) with 44,500 pounds (20,227 kilograms) payload.
C-130H: 23,000 feet (7,077 meters) with 42,000 pounds (19,090 kilograms) payload.
C-130E: 19,000 feet (5,846 meters) with 42,000 pounds (19,090 kilograms) payload
Maximum Takeoff Weight:
C-130E/H/J: 155,000 pounds (69,750 kilograms)
C-130J-30: 164,000 pounds (74,393 kilograms)
Maximum Allowable Payload:
C-130E, 42,000 pounds (19,090 kilograms)
C-130H, 42,000 pounds (19,090 kilograms)
C-130J, 42,000 pounds (19,090 kilograms)
C-130J-30, 44,000 (19,958 kilograms)
Maximum Normal Payload:
C-130E, 36,500 pounds (16,590 kilograms)
C-130H, 36,500 pounds (16,590 kilograms)
C-130J, 34,000 pounds (15,422 kilograms)
C-130J-30, 36,000 pounds (16,329 kilograms)
Range at Maximum Normal Payload:
C-130E, 1,150 miles (1,000 nautical miles)
C-130H, 1,208 miles (1,050 nautical miles)
C-130J, 2,071 miles (1,800 nautical miles)
C-130J-30, 1,956 miles (1,700 nautical miles)
Range with 35,000 pounds of Payload:
C-130E, 1,438 miles (1,250 nautical miles)
C-130H, 1,496 miles (1,300 nautical miles)
C-130J, 1,841 miles (1,600 nautical miles)
C-130J-30, 2,417 miles (2,100 nautical miles)
Maximum Load:
C-130E/H/J: 6 pallets or 74 litters or 16 CDS bundles or 92 combat troops or 64 paratroopers, or a combination of any of these up to the cargo compartment capacity or maximum allowable weight.
C-130J-30: 8 pallets or 97 litters or 24 CDS bundles or 128 combat troops or 92 paratroopers, or a combination of any of these up to the cargo compartment capacity or maximum allowable weight.
Crew: C-130E/H: Five (two pilots, navigator, flight engineer and loadmaster)
C-130J/J-30: Three (two pilots and loadmaster)
Aeromedical Evacuation Role: A basic crew of five (two flight nurses and three medical technicians) is added for aeromedical evacuation missions. Medical crew may be decreased or increased as required by the needs of patients.
Unit Cost: C-130E, $11.9, C-130H, $30.1, C-130J, $48.5 (FY 1998 constant dollars in millions)
Date Deployed: C-130A, Dec 1956; C-130B, May 1959; C-130E, Aug 1962; C-130H, Jun 1974; C-130J, Feb 1999
Inventory: Active force, 145; Air National Guard, 181; Air Force Reserve, 102
PICTURES:
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[multipage=Attack]
A-10 Thunderbolt II:
INFORMATION:
General Characteristics
Primary Function: A-10 -- close air support, A-10C - airborne forward air control
Contractor: Fairchild Republic Co.
Power Plant: Two General Electric TF34-GE-100 turbofans
Thrust: 9,065 pounds each engine
Wingspan: 57 feet, 6 inches (17.42 meters)
Length: 53 feet, 4 inches (16.16 meters)
Height: 14 feet, 8 inches (4.42 meters)
Weight: 29,000 pounds (13,154 kilograms)
Maximum Takeoff Weight: 51,000 pounds (22,950 kilograms)
Fuel Capacity: 11,000 pounds (7,257 kilograms)
Payload: 16,000 pounds (7,257 kilograms)
Speed: 420 miles per hour (Mach 0.56)
Range: 800 miles (695 nautical miles)
Ceiling: 45,000 feet (13,636 meters)
Armament: One 30 mm GAU-8/A seven-barrel Gatling gun; up to 16,000 pounds (7,200 kilograms) of mixed ordnance on eight under-wing and three under-fuselage pylon stations, including 500 pound (225 kilograms) Mk-82 and 2,000 pounds (900 kilograms) Mk-84 series low/high drag bombs, incendiary cluster bombs, combined effects munitions, mine dispensing munitions, AGM-65 Maverick missiles and laser-guided/electro-optically guided bombs; infrared countermeasure flares; electronic countermeasure chaff; jammer pods; 2.75-inch (6.99 centimeters) rockets; illumination flares and AIM-9 Sidewinder missiles.
Crew: One
Unit Cost: Not available
Initial operating capability: A-10A, 1977; A-10C, 2007
Inventory: Active force, A-10, 143 and A-10C, 70; Reserve, A-10, 46 and OA-10, 6; ANG, A-10, 84 and OA-10, 18
PICTURES:
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[multipage=Fighter]
F-22 Raptor:
INFORMATION:
General Characteristics
Primary Function: Air dominance, multi-role fighter
Contractor: Lockheed-Martin, Boeing
Power Plant: Two Pratt & Whitney F119-PW-100 turbofan engines with afterburners and two-dimensional thrust vectoring nozzles.
Thrust: 35,000-pound class (each engine)
Wingspan: 44 feet, 6 inches (13.6 meters)
Length: 62 feet, 1 inch (18.9 meters)
Height: 16 feet, 8 inches (5.1 meters)
Weight: 43,340 pounds (19,700 kilograms)
Maximum Takeoff Weight: 83,500 pounds (38,000 kilograms)
Fuel Capacity: Internal: 18,000 pounds (8,200 kilograms); with 2 external wing fuel tanks: 26,000 pounds (11,900 kilograms)
Payload: Same as armament air-to-air or air-to-ground loadouts; with or without 2 external wing fuel tanks.
Speed: Mach 2 class with supercruise capability
Range: More than 1,850 miles ferry range with 2 external wing fuel tanks (1,600 nautical miles)
Ceiling: Above 50,000 feet (15 kilometers)
Armament: One M61A2 20-millimeter cannon with 480 rounds, internal side weapon bays carriage of two AIM-9 infrared (heat seeking) air-to-air missiles and internal main weapon bays carriage of six AIM-120 radar-guided air-to-air missiles (air-to-air loadout) or two 1,000-pound GBU-32 JDAMs and two AIM-120 radar-guided air-to-air missiles (air-to-ground loadout)
Crew: One
Unit Cost: $143 million
Initial operating capability: December 2005
Inventory: Total force, 137
PICTURES:
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F-15E Strike Eagle:
INFORMATION:
General Characteristics
Primary function: Air-to-ground attack aircraft
Contractor: McDonnell Douglas Corp.
Power plant: Two Pratt & Whitney F100-PW-220 or 229 turbofan engines with afterburners
Thrust: 25,000 - 29,000 pounds each engine
Wingspan: 42.8 feet (13 meters)
Length: 63.8 feet (19.44 meters)
Height: 18.5 feet (5.6 meters)
Weight: 37,500 pounds ( 17,010 kilograms)
Maximum takeoff weight: 81,000 pounds (36,450 kilograms)
Fuel capacity: 35,550 pounds (three external tanks plus conformal fuel tanks)
Payload: depends upon mission
Speed: 1,875 mph (Mach 2.5 plus)
Range: 2,400 miles (3,840 kilometers) ferry range with conformal fuel tanks and three external fuel tanks
Ceiling: 60,000 feet (18,288 meters)
Armament: One 20mm multibarrel gun mounted internally with 500 rounds of ammunition. Four AIM-9 Sidewinder missiles and four AIM-120 AMRAAM, or eight AIM-120 AMRAAM missiles. Any air-to-surface weapon in the Air Force inventory (nuclear and conventional)
Crew: Pilot and weapon systems officer
Unit cost: $31.1 million (fiscal 98 constant dollars)
Initial operating capability: September 1989
Inventory: Total force, 223
PICTURES:
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F-15 Eagle:
INFORMATION:
General Characteristics
Primary function: Tactical fighter
Contractor: McDonnell Douglas Corp.
Power plant: Two Pratt & Whitney F100-PW-100, 220 or 229 turbofan engines with afterburners
Thrust: (C/D models) 23,450 pounds each engine
Wingspan: 42.8 feet (13 meters)
Length: 63.8 feet (19.44 meters)
Height: 18.5 feet (5.6 meters)
Weight: 31,700 pounds
Maximum takeoff weight: (C/D models) 68,000 pounds (30,844 kilograms)
Fuel Capacity: 36,200 pounds (three external plus conformal fuel tanks)
Payload: depends on mission
Speed: 1,875 mph (Mach 2 class)
Ceiling: 65,000 feet (19,812 meters)
Range: 3,450 miles (3,000 nautical miles) ferry range with conformal fuel tanks and three external fuel tanks
Crew: F-15A/C: one. F-15B/D/E: two
Armament: One internally mounted M-61A1 20mm 20-mm, six-barrel cannon with 940 rounds of ammunition; four AIM-9 Sidewinder and four AIM-120 AMRAAMs or eight AIM-120 AMRAAMs, carried externally.
Unit Cost: A/B models - $27.9 million (fiscal 98 constant dollars);C/D models - $29.9 million (fiscal 98 constant dollars)
Initial operating capability: September 1975
Inventory: Total force, 522
PICTURES:
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[multipage=Servailence]
SR-71 Blackbird:
INFORMATION:
General characteristics
* Crew: 2
* Payload: 3,500 lb (1,600 kg) of sensors
* Length: 107 ft 5 in (32.74 m)
* Wingspan: 55 ft 7 in (16.94 m)
* Height: 18 ft 6 in (5.64 m)
* Wing area: 1,800 ft2 (170 m2)
* Empty weight: 67,500 lb (30,600 kg)
* Loaded weight: 170,000 lb (77,000 kg)
* Max takeoff weight: 172,000 lb (78,000 kg)
* Powerplant: 2× Pratt & Whitney J58-1 continuous-bleed afterburning turbojets, 32,500 lbf (145 kN) each
* Wheel track: 16 ft 8 in (5.08 m)
* Wheel base: 37 ft 10 in (11.53 m)
* Aspect ratio: 1.7
Performance
* Maximum speed: Mach 3.2+ (2,200+ mph, 3,530+ km/h, 1,900+ knots) at 80,000 ft (24,000 m)
* Range: 2,900 nmi (5,400 km)
* Ferry range: 3,200 nmi (5,925 km)
* Service ceiling: 85,000 ft (25,900 m)
* Rate of climb: 11,810 ft/min (60 m/s)
* Wing loading: 94 lb/ft² (460 kg/m²)
* Thrust/weight: 0.382
PICTURES:
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Reaper:
INFORMATION:
General Characteristics
* Crew: None
* Landing Type: runway
* Launch Type: runway
* Length: 36 ft (11 m)
* Wingspan: 66 ft (20 m)
* Height: 12.5 ft (3.6 m)
* Empty weight: 4,900 lb (2223 kg)
* Fuel Capacity: 4,000 lb (1,800 kg)
* Max takeoff weight: 10,500 lb (4760 kg)
* Power Plant: Honeywell TPE331-10 turboprop engine, 900 shp (671 kW), with Digital Electronic Engine Control (DEEC)[60]
Performance
* Maximum speed: 260 knots (482 km/h, 300 mph)
* Cruise speed: 150–170 knots (276–313 km/h, 172–195 mph)[61]
* Range: 3,200 nmi (5,926 km, 3,682 mi)
* Endurance: 14–28 hours (14 hours fully loaded)[62]
* Payload: 3,800 lb (1,700 kg)
o Internal: 800 lb (360 kg)
o External: 3,000 lb (1,400 kg)
* Service ceiling: 50,000 ft (15 km)
* Operational altitude: 25,000 ft (7.5 km)[63]
Sensors
* AN/APY-8 Lynx II radar[64]
* AN/DAS-1 MTS-B Multi-Spectral Targeting System [65]
Armament
* 7 Hardpoints
o Up to 1,500 lb (680 kg) on the two inboard weapons stations[66]
o Up to 750 lb (340 kg) on the two middle stations[66]
o Up to 150 lb (68 kg) on the outboard stations [66]
o Center station not used
* Up to 14 AGM-114 Hellfire air to ground missiles can be carried or four Hellfire missiles and two 500 lb (230 kg) GBU-12 Paveway II laser-guided bombs. The 500 lb (230 kg) GBU-38 Joint Direct Attack Munition (JDAM) can also be carried. Testing is underway to support the operation of the AIM-92 Stinger air-to-air missile.
PICTURES:
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Global Hawk:
INFORMATION:
General characteristics
* Crew: 0
* Length: 44 ft 5 in (13.54 m)
* Wingspan: 116 ft 2 in (35.41 m)
* Height: 15 ft 2 in (4.62 m)
* Empty weight: 8,490 lb (3,851 kg)
* Gross weight: 22,900 lb (10,387 kg)
* Powerplant: 1 × Allison Rolls-Royce AE3007H turbofan engine, 7,050 lbf (31.4 kN) thrust
Performance
* Maximum speed: 497.1 mph (800.0 km/h; 432.0 kn)
* Cruise speed: 404 mph (351 kn; 650 km/h)
* Range: 15,525 mi (13,491 nmi; 24,985 km)
* Endurance: 36 hours
* Service ceiling: 65,000 ft (19,812 m)
PICTURES:
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PREDATOR:
INFORMATION:
General characteristics
* Crew: none on-board
* Length: 27 ft (8.22 m)
* Wingspan: 48.7 ft (14.8 m); MQ-1B Block 10/15: 55.25 ft (16.84 m)
* Height: 6.9 ft (2.1 m)
* Wing area: 123.3 sq ft[55] (11.5 m²)
* Empty weight: 1,130 lb[54] (512 kg)
* Loaded weight: 2,250 lb (1,020 kg)
* Max takeoff weight: 2,250 lb[54] (1,020 kg)
* Powerplant: 1× Rotax 914F turbocharged four-cylinder engine, 115 hp[54] (86 kW)
Performance
* Maximum speed: 135 mph (117 knots, 217 km/h)
* Cruise speed: 81–103 mph (70–90 knots, 130–165 km/h)
* Stall speed: 62 mph (54 knots, 100 km/h) (dependent on aircraft weight)
* Range: >2,000 nmi (2,300 mi/3,700 km) [56]
* Endurance: 24 hours[1]
* Service ceiling: 25,000 ft[54] (7,620 m)
Armament
2 hardpoints
* 2 × AGM-114 Hellfire (MQ-1B)
* 4 × AIM-92 Stinger (MQ-1B)
* 6 × Griffin air-to-surface missiles[57]
Avionics
* ASIP-1C
* AN/AAS-52 Multi-Spectral Targeting System
* AN/ZPQ-1 Synthetic Aperture Radar (early airframes only)
PICTURES:
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[multipage=Helicopter]
Pave Low:
INFORMATION:
General characteristics
* Crew: 6 (two pilots, two flight engineers and two aerial gunners)
* Capacity: 37 troops (55 in alternate configuration)
* Length: 88 ft (28 m)
* Rotor diameter: 72 ft (21.9 m)
* Height: 25 ft (7.6 m)
* Empty weight: 32,000 lb (14,515 kg)
* Max takeoff weight: 46,000 lb (50,000 lb in war time) (21,000 kg)
* Powerplant: 2× T64-GE-100 turboshaft, 4,330 shp (3,230 kW) each
* Rotor system: 6 blades
Performance
* Maximum speed: 170 knots (196 mph, 315 km/h)
* Cruise speed: 150 kt (173 mph, 278 km/h)
* Range: 600 nmi (1,100 km) can be extended with in-flight refueling
* Service ceiling: 16,000 ft (4,900 m)
Armament
* Any combination of three 7.62 mm M134 Miniguns and/or .50 BMG (12.7 mm) M2 Browning machine guns mounted on left and right sides (immediately behind flight deck) and ramp
PICTURES:
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The following user thanked TheWraith-- for this useful post:
02-18-2011, 01:14 AM
#12
TheWraith--
Gym leader
02-18-2011, 01:35 AM
#14
TheWraith--
Gym leader
02-18-2011, 01:45 AM
#16
TheWraith--
Gym leader
02-18-2011, 02:06 AM
#19
TheWraith--
Gym leader
Originally posted by Unsuccessful
Its been like 8 years to be exact, and it was because of Mr. Dr. George W. Bush and 9/11 But Saudi Arabia were the ones that did 9/11.
well i know its been a while. and oh yeah i remember that now. yeah that is true
---------- Post added at 09:06 PM ---------- Previous post was at 08:50 PM ----------
Originally posted by ps3kilz
ROTC IS FOR homos marines all the way
dude im 15
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