NationStates Jolt Archive

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General characteristics

Crew: 1
Length: 62 ft 1 in (18.90 m)
Wingspan: 44 ft 6 in (13.56 m)
Height: 16 ft 5 in (5.08 m)
Wing area: 840 ft² 78.04 m²
Empty: 31,670 lb (14,365 kg)
Loaded: 60,000 lb (27,216 kg)
Maximum takeoff: 80,000 lb (36,500 kg)
Powerplant: 2x Pratt & Whitney F119-PW-100 turbofans, 35,000 lbf (156 kN) thrust each

Performance:

Maximum speed: Mach 1.8+
Cruising Speed: Mach 1.5
Range: miles ( km)
Service ceiling: 60,000 ft (18,288 m)
Rate of climb: ft/min ( m/min)
Wing loading: lb/ft² ( kg/m²)
Thrust/weight:

Armament:

Gun: 1x M61A2 Vulcan 20 mm Gatling gun with 480 rounds
Missiles: 6x AIM-120C AMRAAM, 2x AIM-9 Sidewinder
Bombs: 2x JDAM
4x external hardpoints can be fitted to carry weapons or fuel tanks, each with a capacity of 5,000 lb (2,270 kg)

General characteristics:

Crew: 2
Length: 69 ft (21 m)
Wingspan: 172 ft (52.1 m)
Height: 17 ft (5.1 m)
Wing area: 5,000 ft² (460 m²)
Empty: 158,000 lb (71,700 kg)
Loaded: 336,500 lb (152,600 kg)
Maximum takeoff: 336,500 lb (152,600 kg)
Powerplant: 4× General Electric F-118-GE-100 turbofans; 17,300 lbf (77kN) thrust each

Performance:

Maximum speed: Mach 0.85
Maximum speed: 560 knots (1,000 km/h)
Range: 6,500 nmiles (12,000 km)
Service ceiling: 50,000 ft (15,152 m)
Rate of climb: ft/min (m/min)
Wing loading: 67.3 lb/ft² (329 kg/m²)
Thrust/weight ratio: 0.205:1

Armament:

40,000 lb (18,000 kg) of bombs

General characteristics:

Crew: 4 (aircraft commander, copilot, offensive systems officer and defensive systems officer)
Length: 147 ft (44.81 m)
Wingspan: 136 ft 8.5 in (41.67 m) extended, 78 ft 2.5 in (23.84 m) swept
Height: 34 (10.36 m)
Wing area: 1,950 ft² 181.2 m²
Empty: 192,000 lb (87,100 kg)
Loaded: 326,000 lb (148,000 kg)
Maximum takeoff: 477,000 lb (216,000 kg)
Powerplant: 4× General Electric F101-GE-102 turbofans; 14,600 ibf (64.94 kN) thrust dry; 30,780 lbf (136.92 kN) thrust with afterburning

Performance:

Maximum speed: Mach 1.25
Maximum speed: 717 knots (1,329 km/h)
Range: 1,267 miles (2,037 km)
Service ceiling: 60,000 ft (18,300 m)
Rate of climb: ft/min ( m/min)
Wing loading: 167 lb/ft² (816 kg/m²)
Thrust/weight ratio: 0.37:1

Armament:

3 internal bays for 75,000 lb (34,000 kg), options include
84× Mk-82 general purpose bombs
84× Mk-62 naval mines
30× CBU-87/89 cluster munitions
30× CBU-97 sensor fused weapons
24× GBU-31 JDAM GPS guided bombs
24× Mk-84 general purpose bombs
6 external hardpoints for an additional 59,000 lb (27,000 kg) of ordinance

General characteristics:

Crew: 5
Length: 159 ft 4 in (48.5 m)
Wingspan: 185 ft 0 in (56.4 m)
Height: 40 ft 8 in (12.4 m)
Wing area: 4,000 ft² (370 m²)
Empty: 195,000 lb (88,500 kg)
Loaded: 265,000 lb (120,000 kg)
Maximum takeoff: 488,000 lb (220,000 kg)
Powerplant: 8× Pratt & Whitney TF33-P-3/103 turbofans; 17,000 lbf (76.62 kN) thrust

Performance:

Maximum speed: 650 mph (1,000 km/h)
Combat range: 4,300 miles (6,900 km)
Ferry range: miles ( km)
Service ceiling: 47,000 ft (14,300 m)
Rate of climb: ft/min ( m/min)
Wing loading: 30 lb/ft² (150 kg/m²)
Thrust/weight ratio: 0.51:1

Armament:

70,000 lb (32,000 kg) of bombs

General characteristics:

Crew: 1
Length: 65 ft 11 in (20.08 m)
Wingspan: 43 ft 4 in (13.20 m)
Height: 12 ft 5 in (3.78 m)
Wing area: 780 ft² (73 m²)
Empty: 29,500 lb (13,380 kg)
Loaded: 52,500 lb (23,814 kg)
Maximum takeoff: lb ( kg)
Powerplant: 2x General Electric F404-F1D2 turbofans, 10,600 lbf (48.0 kN) thrust each

Performance:

Maximum speed: km/h ( mph)
Range: 800 nautical miles (1,500 km)
Service ceiling: ft ( m)
Rate of climb: ft/min ( m/min)
Wing loading: lb/ft² ( kg/m²)
Thrust/weight:

Armament:

2x internal weapons bays with one hardpoint each (total of 2 weapons) including:
Bombs: BLU-109 hardened penetrator, GBU-10 Paveway II laser-guided, GBU-27 laser-guided
Missiles: AGM-65 Maverick air-to-surface, AGM-88 HARM air-to-surface

General characteristics:

Crew: pilot
Length: 50 ft 6 in (15.37 m)
Wingspan: 35 ft 0 in (10.65 m)
Height: 17 ft 4 in (5.28 m)
Wing area: 459.6 ft² (42.7 m²)
Empty: 26,455 lb (12,000 kg)
Loaded: 41,900 lb (19,000 kg)
Maximum takeoff: 50,000 lb (22,680 kg)
Powerplant:
Primary: 1x Pratt & Whitney F135 afterburning turbofan 37,200 lbf (165 kN) thrust
Lift fan (STOVL): 1x General Electric/Rolls-Royce F136 18,000 lbf (80 kN) thrust

Performance:

Maximum speed: km/h ( mph) Mach 1.8
Range: 620 miles (1000 km) without drop tanks
Service ceiling: 48,000 ft (15,000 m)
Rate of climb: m/min ( ft/min)
Wing loading: 91.4 lb/ft² (446 kg/m²)
Thrust/weight: 6.2 N/kg

Armament:

1x GAU-12/U 25 mm cannon (internal with 180 rounds in F-35A, as an external pod with 220 rounds in F-35B/C)
4 AAMs with a mix of AIM-9X, AIM-132 ASRAAM and AIM-120 AMRAAM(mounted within two internal weapons bays)
At the expense of stealth, several more weapons (missles/bombs) can be attached to the aircraft via pylons on the wings.

Note: This is for F-35A and F-35C. The F-35B is currently not for sale.

General characteristics:

Crew: 1 (A/C), 2 (B/D/E)
Length: 63.75 ft (19.43 m)
Wingspan: 42.75 ft (13.03 m)
Height: 18.625 ft (5.68 m)
Wing area: 608 ft² (56.5 m²)
Empty: 28,000 lb (12,700 kg)
Loaded (C variant): 44,500 lb (20,200 kg)
Maximum takeoff:
C/D: 68,000 lb (30,800 kg)
E: 81,000 lb (36,700 kg)
Powerplant: Engine types
F-15E: 2x Pratt & Whitney F100-100 afterburning turbofans, 23,930 lbf (106.4 kN) thrust each
F-15K: 2x General Electric F110-GE-129 afterburning turbofans, 29,000 lbf (129 kN) thrust each

Performance:

Maximum speed: 1,650 mph (2,660 km/h) (Mach 2.5)
Range: km ( miles)
Service ceiling:
A/B/C/D: 65,000 ft (19,800 m)
E: 50,000 ft (15,000 m)
Rate of climb: 50,000 ft/min (15,240 m/min)
Wing loading: lb/ft² ( kg/m²)
Thrust/weight:

Armament:

2 wing and 1 centerline hardpoints for a total of 16,000 lb (7,300 kg) ordinance, including:
Guns: 1x M61 Vulcan 20 mm Gatling gun with 940 rounds (A/B/C/D), 500 rounds (E)
Missiles: 4x AIM-7F (upgraded to AMRAAM), 4x AIM-9 Sidewinders on wing plyons, plus a total ordnance load of 16,000 lb (7,300 kg) on two wing stations and one centerline station
Bombs: The F-15E is capable of carrying every air to ground bomb in the USAF inventory, including free fall nuclear bombs and the 4,500 lb GBU-28 bunker penetration bomb.

Crew: one, pilot
First Flight: August 27, 1990
Manufacturer: Northrop, McDonnell-Douglas

Dimensions:

Length: 67 ft 5 in 20.60 m
Wingspan: 43 ft 7 in 13.30 m
Height: 13 ft 11 in 4.30 m
Wing area: 948 ft² 88m²

Weights

Empty: 32,934 lb 14,970 kg
Loaded: 51,320 lb 23,327 kg
Maximum takeoff: 64,000 lb 29,029 kg
Powerplant:
Engines Tested with both
2x General Electric YF120 or
2x Pratt & Whitney YF119
Thrust 60,000 lbf 277 kN

Performance:

Maximum speed: 1,400+ mph 2,240+ km/h Mach 2+
Supercruise speed: Mach 1.8 +
Unrefuelled range: 921 miles 1,474 km
Service ceiling: 65,000+ ft 19,800+ m
Rate of climb ft/min m/min:
Wing loading: 54 lb/ft² 265 kg/m²
Thrust/Weight: 1.4:1

Armament:

Guns: 1x 20 mm M61 Vulcan cannon
Missiles:
Up to 6x from a mix of
AIM-7 Sparrow
AIM-120 AMRAAM
AIM-9 Sidewinder

Role: Air-to-ground attack aircraft
Crew: 2
First flight:
Entered service: April 1988
Manufacturer: McDonnell Douglas Corp.

Dimensions:

Length: 63.8 ft 19.43 m
Wingspan: 42.8 ft 13.06 m
Height: 18.5 ft 5.69 m
Wing area: 608 ft² 56.5 m²

Weights:

Empty: 28,000 lb 12,700 kg
Loaded: lb kg
Maximum takeoff: 81,000 lb 36,700 kg

Powerplant:

Engines: 2 x Pratt & Whitney F100-PW-229 afterburning turbofans
Thrust: 29,000 pounds-force 129 kN (each)

Performance:

Maximum speed: Mach 2.5+
Combat range:
Ferry range: 2,400 miles 3,900 km
Service ceiling: 65,000 ft 19,800 m
Rate of climb: 50,000 ft/min 15,000 m/min
Cost: $31.1 million (1998 Dollars)

Armament:

Guns: 1x M61 Vulcan 20 mm cannon with 512 rounds
Bombs CBU-52, CBU-58, CBU-71, CBU-87 cluster, CBU-89 Gator, CBU-90, CBU-92, CBU-93, Mk 20 Rockeye, GBU-10 Paveway II, GBU-12 Paveway II, GBU-15 Capable of delivering nuclear ordinance.
Missiles: AIM-7 Sparrow, AIM-9M Sidewinder, AIM-120 AMRAAM, AGM-45 Shrike, AGM-65 Maverick, AGM-88 HARM

General characteristics:

Crew: 1 (A/C), 2 (B/D)
Length: 47 ft 8 in (14.52 m)
Wingspan: 31 ft (9.45 m)
Height: 16 ft 8 in (5.09 m)
Wing area: 300 ft² (27.87 m²)
Empty: 18,238 lb (8,272 kg)
Loaded: 26,463 lb (12,003 kg)
Maximum takeoff: 42,300 lb (19,187 kg)
Powerplant:
F-16A/B: Pratt & Whitney F100-PW-200 turbofan, 14,670 lbf (64.9 kN), afterburning 23,830 lbf (106.0 kN)
F-16C/D:
Block 25/32/42: Pratt & Whitney F100-PW-220 turbofan, 14,590 lbf (64.9 kN), afterburning 23,770 lbf (105.7 kN)
Block 30/40: General Electric F110-GE-100 turbofan, 17,155 lbf (76.3 kN), afterburning 28,984 lbf (128.9 kN)
Block 50: General Electric F110-GE-129 turbofan, 17,155 lbf (76.3 kN), afterburning 28,984 lbf (128.9 kN)
Block 52: Pratt & Whitney F100-PW-229 turbofan, 17,000 lbf (75.6 kN), afterburning 28,500 lbf (127 kN)
F-16E/F: General Electric F110-GE-132 turbofan, 19,000 lbf (84.5 kN), afterburning 32,500 lbf (144.6 kN)

Performance:

Maximum speed: 1,350 mph (2,173 km/h)
Range: 340 miles (547 km)
Service ceiling: 50,000 ft (15,240 m)
Rate of climb: 50,000 ft/min 15,240 m/min
Wing loading: lb/ft² (kg/m²)
Thrust/weight:

Armament:

Guns: M61 Vulcan 20 mm Gatling gun
Rockets: CRV-7
Missiles:
Air-to-air: AIM-9 Sidewinder, AIM-120 AMRAAM
Air-to-ground: AGM-65 Maverick, AGM-88 HARM
Anti-ship: AGM-119 Penguin
Bombs: CBU-87 cluster, CBU-89 gator mine, CBU-97, Paveway, JDAM, Mk 80 series

General characteristics:

Crew: 1(A/C) 2(B/D)
Unit Cost: $39.5 Million
Contractor: Prime: McDonnell Douglas; Major Subcontractor: Northrop
First flight:
November 1978
November 1995 (E/F models)
Operational:
October 1983 (A/B models)
September 1987 (C/D models)
September 2001 (E/F models)

Dimensions:

Length: 56 ft 4 in (17.1 m)
Wingspan: 40 ft (12.3 m)
Height: 15 ft 4 in (4.7 m)
Wing area: 300 ft² (27.87 m²)

Weights:

Empty: 12,500 lb (5,700 kg)
Loaded: lb ( kg)
Maximum Takeoff: 29,750 lb (13,400 kg)

Powerplant:

Engine: 2x General Electric F404-GE-402 enhance performance turbofans
Thrust: 17,700 lbf per engine (79 kN) thrust

Performance:

Maximum speed: Mach 1.8+
Service ceiling: 50,000 ft (15,000 m)
Thrust/weight: >1

Armament:

Guns: M61 Vulcan 20 mm Gatling gun
Missiles:
Air-to-air: AIM-9 Sidewinder, AIM-120 AMRAAM
Air-to-ground: AGM-45_Shrike, AGM-65 Maverick, AGM-88 HARM, SLAM-ER, JSOW
Anti-ship: AGM-84 Harpoon
Bombs: CBU-87 cluster, CBU-89 gator mine, CBU-97, Paveway, JDAM, Mk 80 series

General characteristics:

Crew: 2 (Pilot and Radar Intercept Officer)
Length: 61 ft 9 in (18.6 m)
Wingspan: 64 ft (19 m) unswept, 38 ft (11.4 m) swept
Height: 16 ft (4.8 m)
Wing area: 565 ft² (54.5 m²)
Empty: lb ( kg)
Loaded: lb ( kg)
Maximum takeoff: 72,900 lb (32,805 kg)
Powerplant:
F-14A: 2x Pratt & Whitney TF-30P-414A turbofans, 15,285 lbf (68 kN) each, 20,900 lbf (93 kN) with afterburner
F-14B/D: 2x General Electric F110-GE-400 turbofans, 16,610 lbf (74 kN) each, 27,000 lbf (120 kN) with afterburner

Performance:

Maximum speed: 1,544 mph (2,485 km/h) Mach 2.34
Range: 576 miles (927 km)
Service ceiling: 50,000+ ft (15,000+ m)
Rate of climb: 30,000 ft/min (9,145 m/min)
Wing loading: 113.4 lb/ft² (553.9 kg/m²)
Thrust/weight: 0.72:1

Armament:

13,000 lb (5,900 kg) of ordinance including;
Guns: 1x M61 Vulcan 20 mm Gatling Gun
Missiles: AIM-54 Phoenix, AIM-7 Sparrow and AIM-9 Sidewinder air-to-air
Loading configurations:
2x AIM-9 + 6x AIM-54
2x AIM-9 + 2x AIM-54 + 3x AIM-7
2x AIM-9 + 4x AIM-54 + 2x AIM-7
2x AIM-9 + 6x AIM-7
Bombs: Air-to-ground precision strike ordnance

General characteristics:

Crew: 1
Length: 53 ft 4 in (16.16 m)
Wingspan: 57 ft 6 in (17.42 m)
Height: 14 ft 8 in (4.42 m)
Wing area: 506 ft² (47 m²)
Empty: 21,519 lb (9,761 kg)
Loaded: 32,730 lb (14,846 kg)
Maximum takeoff: 51,000 lb (23,000 kg)
Powerplant: 2x General Electric TF34-GE-100 turbofans, 9,065 lbf (40.32 kN) thrust (each)

Performance:

Maximum speed: 420 mph (676 km/h)
Range: 620 miles (1,000 km)
Service ceiling: 45,000 feet (13,600 m)
Rate of climb: 6,000 ft/min (1,830 m/min)
Wing loading: kg/m² ( lb/ft²)
Thrust/weight:

Armament:

The GAU-8/A "Avenger" Gatling gun assembly next to a VW Beetle1x 30 mm GAU-8/A Avenger seven-barrel Gatling gun with 1,174 rounds
8x underwing and 3x under-fuselage pylon stations holding 16,000 lb (7,300 kg) housing:
Mk 82, Mk 83, and Mk 84 general-purpose bombs
BLU-1, BLU-27/B Rockeye II and CBU-52/71 cluster bombs
AGM-65 Maverick and AIM-9 Sidewinder Missiles
Hydra 70 mm and 127 mm rocket pods
Illumination flares, ECM and chaff pods

General characteristics:

Crew: 13
5 Officers: pilot, co-pilot, navigator, fire control officer, electronic warfare officer
8 Enlisted: flight engineer, TV operator, infrared detection set operator, loadmaster, four aerial gunners
Length: 97 ft 9 in (29.8 m)
Wingspan: 132 ft 7 in (40.4 m)
Height: 38 ft 10 in (11.9 m)
Wing area: ft² (m²)
Empty: lb ( kg)
Loaded: lb (kg )
Maximum takeoff: 155,000 lb (69,750 kg)
Powerplant: 4x Allison T56-A-15 turboprops, 4,910 shaft hp (3,700 kW) each

Performance:

Maximum speed: 300 mph (483 km/h) Mach .4
Range: 2,200 nautical miles (4,070 km) (AC-130H: 1,300 nautical miles (2,400 km))
Service ceiling: 30,000 ft (9,144 m) (AC-130H: 25,000 ft (7,576 m))
Rate of climb: ft/min ( m/min)
Wing loading: lb/ft² ( kg/m²)
Power/mass:

Armament:

1x GAU-12 Equalizer 25mm Gatling gun (AC-130H: 2x M61 Vulcan 20 mm Gatling guns)
1x L60 Bofors 40 mm rapid-fire single-barrel autocannon
1x M102 105 mm howitzer
Note: The two M61 Vulcan cannons were removed from the AC-130H around 2002. They, along with the L60 Bofors are being replaced by two M-242 25mm chain guns. The AC-130U is also replacing the GAU-12 and L-60 with two 25mm M-242's.

Description:

Role: Heavy strategic airlift transport
Crew: 7 (pilot, copilot, two flight engineers, three loadmasters)

Dimensions:

Length: 247.1 ft 75.3 m
Wingspan: 222.9 ft 67.89 m
Height: 65.1 ft 19.84 m
Wing area: 6,200 ft² 576 m²

Weights:

Empty: 337,937 lb 153,285 kg
Loaded: 769,000 lb 348,810 kg
Maximum take-off: 840,000 lb 381,024 kg

Powerplant:

Engines: Four General Electric TF39-1 turbofans
Thrust: 43,000 lbf 191 kN

Performance:

Maximum speed: 570 mph 917 km/h
Combat range: 3,749 mi 6,033 km
Ferry range: 7,991 mi 12,860 km
Service ceiling: 34,000 ft 10.36 km
Rate of climb: 1,800 ft/min 549 m/min

Description:

Role: Cargo and troop transport
Crew: 5 to 6
First flight: 1963
Manufacturer: Lockheed-Georgia Co., Marietta, Georgia

Dimensions:

Length: 145 ft 0 in (C-141A)
168 ft 4 in (C-141B) 44.2 m
51.3 m
Wingspan: 160 ft 0 in 48.8 m
Height: 39 ft 3 in 12 m
Wing area: 3,228 ft² 300 m²

Weights:

Empty: 144,492 lb (C-141B) 65,542 kg
Loaded:
Maximum takeoff: 316,600 lb (C-141A)
323,100 lb (C-141B) 143,607 kg
147,000 kg

Powerplant:

Engines: 4 × Pratt & Whitney TF33-P-7 turbofans
Thrust: 20,250 lbf each 90.1 kN each

Performance:

Maximum speed: 571 mph (C-141A)
567 mph (C-141B) 919 km/h
912 km/h
Combat range: 4,080 miles (C-141A)
2,935 miles (C-141B) 6,566 km
4,723 km
Ferry range: 6,140 miles (C-141B) 9,880 km
Service ceiling: 41,000 ft (C-141B) 12,500 m
Rate of climb: 2,600 ft/min (C-141B) 792 m/min

Role: Cargo and Troop Transport
Crew: Three (2 Pilots, 1 Loadmaster)
First flight:
Entered service: June 1993
Manufacturer: Boeing Integrated Defense Systems
Length: 174 ft 53 m
Wingspan: 169.8 ft 58 m
Height: 55.1 ft 16.8 m
Wing area: 3,800 ft² 353 m²
Cargo hold dimensions: 68.2 × 18 × 12.3 ft 20.8 × 5.5 × 3.8 m
Empty: lb kg
Loaded: lb kg
Maximum takeoff: 585,000 lb (current)
630,000 lb. (in testing) 265,500 kg
285,750 kg
Cargo: 170,900 lb 77,500 kg
Capacity: 102 troops/paratroops; 36 litter and 54 ambulatory patients with attendants
Engines: 4 × Pratt and Whitney F117-PW-100 turbofan engines
Thrust: 40,440 lbf 180 kN
Maximum speed: 450 knot 830 km/h
Combat range: 2,400 nautical mile (base)
2,800 nautical mile (ER) 4,400 km
5,200 km
Ferry range: 6,250 nautical mile 11,600 km
Service ceiling: 45,000 ft 13,700 m
Rate of climb: ft/min m/min

Description:

Role: Airborne Warning and Control System (AWACS)
Crew: Flight crew of 4, plus 13-19 mission specialists
First Flight: October 1975
Entered Service: March 1977
Manufacturer: Boeing

Dimensions:
Length: 152 ft 11 in 44.61 m
Wingspan: 145 ft 9 in 44.42 m
Height: 41 ft 4 in 12.6 m
Wing Area: 3,050 ft² 283.4 m²

Weights:

Empty: 162,000 lb 73,480 kg
Loaded: 325,000 lb 147,400 kg
Maximum Takeoff: 347,000 lb 156,000 kg
Capacity:

Powerplant:

Engines: US/NATO: Four Pratt and Whitney TF33-PW-100A turbofan engines
Thrust: (P&W) 4 x 21,000 lbf 4 x 93 kN


Performance:

Maximum Speed: 530 mph 855 km/h
Combat Range: 1,000 miles 1,610 km
Ferry Range: miles km
Service Ceiling: 29,000 ft 9,000 m
Rate of Climb: ft/min m/min
Wing Loading: lb/ft² kg/m²
Thrust/Weight:

Description:

Role: Mid-air refueling
Crew: 3-6 (pilot, copilot, flight engineer + 3 refueling crew)

Dimensions:

Length: 181 ft 7 in 55.35 m
Wingspan: 165 ft 4 in 50.4 m
Height: 58 ft 1 in 17.7 m
Wing area: 3,958 ft² 367.7 m²

Weights:

Empty: 241,027 lb 109,328 kg
Loaded:
Maximum take-off: 590,000 lb 267,620 kg

Powerplant:

Engines: 3 F103/General Electric CF6-50C2 turbofans
Thrust: 52,500 lbf (static) 234 kN

Performance:

Maximum speed: 610 mph 982 km/h
Combat range: 4,370 mi 7,032 km
Ferry range: 11,500 mi 18,507 km
Service ceiling: 33,400 ft 10,180 m
Rate of climb: 6,870 ft/min 34.89 m/s

Primary Function: Aerial refueling and airlift
Prime Contractor: The Boeing Company
Power Plant: KC-135R/T, CFMI CFM56 turbofan engines; KC-135E, Pratt & Whitney TF-33-PW-102 turbofan engines
Thrust: KC-135R, 21,634 lbf (96.233 kN) each engine; KC-135E, 18,000 lbf (80 kN) each engine
Wingspan: 130 ft 10 in (39.88 m)
Length: 136 ft 3 in (41.53 m)
Height: 41 ft 8 in (12.7 m)
Speed: 530 statute miles per hour (850 km/h) at 30,000 ft (9,100 m)
Ceiling: 50,000 ft (15,200 m)
Range: 1,500 statute miles (2,400 km) with 150,000 lb (68,000 kg) of transfer fuel; ferry mission, up to 17,766 km (11,039 statute miles)
Maximum takeoff weight: 322,500 lb (146,300 kg)
Maximum transfer fuel load: 200,000 lb (90,700 kg)
Maximum fuel transfer rate: appr. 6500 lb/min (3000 kg/min) using the boom; appr. 1500 lb/min (700 kg/min) with drogue attached
Maximum cargo capability: 83,000 lb (37,600 kg), 37 passengers
Pallet positions: 6
Crew: four: pilot, co-pilot, navigator, boom operator. Aircraft equipped with PACER CRAG do not have a navigator on most missions. Navigator suites can be installed for unique missions.
Unit cost: US$26 million
Date deployed: August 1956

Description:

Role: Air-to-air refueling
Crew: 2 pilots & AAR operator
Primary contractor: Boeing Integrated Defense Systems
Date Deployed: 2004

Dimensions:

Length: 159 ft 2 in 48.5 m
Wingspan: (to winglet tips) 156 ft 1 in 47.6 m
Height: 52 ft 15.8 m
Cargo: 2,875 ft³ 81.4 m³

Weights:

Dry: 188,705 lb 85,595 kg
Loaded: 284,110 lb 128,870 kg
Max. peace-time take-off weight: 412,000 lb 186,880 kg

Powerplant:

Engines: Two GE CF6-80C2 turbofan engines
Thrust: 63,500 lbf each 282 kN each
Engines Two P&W PW4000 turbofan engines
Thrust 62,000 lbf each 275 kN each
Note: Either one can be picked but the P&W costs $120,000 less than the GE engine.

Performance:

Maximum speed kt: Mach 0.86
Ferry range: 9,250 km / Global, with in-flight refueling
Service ceiling: 40,100 ft 12,200 m

Role: Multirole airlift transport, + many special variants
Crew: Varies, usually 3–5
First flight: August 1954
Entered service: April 1956
Manufacturer: Lockheed Martin Aeronautics
Length: 97 ft 9 in 29.8 m
Wingspan: 132 ft 7 in 40.4 m
Height: 38 ft 10 in 11.9 m
Wing area: 1,745 ft² 162.1 m²
Cargo hold dimensions: ft in x ft in x ft in m x m x m
Empty: 72,892 lb 33,063 kg
Loaded: 155,000 lb 70,310 kg
Maximum takeoff: 175,000 lb 79,380 kg
Capacity:
Engines: 4 Allison T56 turboprops (A-H models)
4 Rolls-Royce AE2100 turboprops
Power: 4 x 4,910 hp 4 x 3,600 kW
Maximum speed: 386 mph 621 km/h
Combat range: 2,490 miles 4,000 km
Ferry range: 4,605 miles 7,410 km
Service ceiling: 23,000 ft 7,010 m
Rate of climb: 1,900 ft/min 580 m/min
Wing loading: lb/ft² kg/m²

Role: High altitude reconnaissance
Crew: one
Length: 62 ft 9 in (R model) 19.1 m
Wingspan: 103 ft (R) 30.9 m
Height: 16 ft 1 in (R) 4.8 m
Wing area: 1,000 ft² 92.9 m²
Empty: 14,990 lb (R) 6,800 kg
Loaded:
Maximum take-off: 41,000 lb (R) 18,600 kg
Engines: One Pratt & Whitney J75-P-13B engine; one General Electric F-118-101 engine
Thrust: 17,000 lbf 76 kN
Maximum speed: 510 mph (R) 821 km/h
Combat range: 3,500 mi (R) 5,633 km
Ferry range :
Service ceiling: > 70,000 ft
(R model 90,000 ft) > 21,212 m
(R 27,432 m)
Rate of climb:

General characteristics:

Crew: 2
Length: 107 ft 5 in (32.7 m)
Wingspan: 55 ft 7 in (16.9 m)
Height: 18 ft 6 in (5.6 m)
Wing area: 1,800 ft² (170 m²)
Empty: 65,000 lb (29,000 kg)
Loaded: 170,000 lb (77,000 kg)
Maximum takeoff: lb ( kg)
Powerplant: 2× Pratt & Whitney J58-1 continuous bleed-afterburning turbojets; 32,500 lbf (145 kN) thrust

Performance:

Maximum speed: Mach 3.32
Maximum speed: 2,193 knots (4,062 km/h)
Combat range: 2,900 miles (5,400 km)
Ferry range: miles ( km)
Service ceiling: 85,000 ft (26,000 m)
Rate of climb: ft/min ( m/min)
Wing loading: 94 lb/ft² (460 kg/m²)
Thrust/weight ratio: 0.382:1