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Military


C-37A Gulfstream V

Specifications
Primary Function Special Air Missions
Builder Gulfstream Aerospace Corporation
Performance
Maximum Range
(Mach 0.80, 8 passengers, 4 crew, NBAA IFR reserves)
6,500 nm 12,046 km
Long Range Cruise Speed Mach 0.80, 459 ktas, 851 km/h
Mmo (Maximum Allowable Mach Number) Mach 0.885
Takeoff Distance (SL, ISA, MTOW) 5,990 ft 1,826 m
Landing Distance (SL, ISA, MLW) 3,170 ft 966 m
Initial Cruise Altitude 41,000 ft 12,497 m
Maximum Cruise Altitude 51,000 ft 15,545 m

Weights
Maximum Takeoff Weight 90,500 lb 41,051 kg
Maximum Landing Weight 75,300 lb 34,156 kg
Maximum Zero Fuel Weight 54,500 lb 24,721 kg
Basic Operating Weight (including 4 crew) 48,000 lb 21,773 kg
Maximum Payload 6,500 lb 2,948 kg
Payload with Maximum Fuel 1,600 lb 726 kg
Maximum Fuel Weight 41,300 lb 18,734 kg
Allowance for outfitting and operating items 8,500 lb 3,856 kg

Design Standards
Engines (2) BMW Rolls-Royce BR710
Rated Takeoff Thrust ea. 14,750 lb 65.6 kN
Passengers (Maximum) 19
Passengers (Typical Outfitting) 13-15
Cabin Pressure Differential 10.17 psid, 6,000 ft cabin at 51,000 ft

Interior
Cabin Length 50 ft 1 in 15.3 m
Cabin Height 6 ft 2 in 1.9 m
Cabin Width 7 ft 4 in 2.2 m
Cabin Volume 1,669 cu ft 47.3 cu m
Baggage Compartment Volume 226 cu ft 6.4 cu m

Exterior
Length 96 ft 5 in 29.4 m
Height 25 ft 10 in 7.9 m
Wingspan 93 ft 6 in 28.5 m
Inventory Active Force, 2 (Andrews AFB); ANG, 0; Reserve, 0
Unit Cost $36 million



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Page last modified: 07-07-2011 02:28:35 ZULU