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The GV statistics and specifications appear courtesy of Gulfstream. For more information about Gulfstream and the GV, visit the Gulfstream website at www.gulfstream.com.
The following specifications are for a production aircraft and some of these (e.g., maximum payload, range) are different for the delivered research aircraft. Users should consult the GV Investigator's Handbook for detailed information on HIAPER's preformance characteristics.
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Aircraft Performance
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Maximum Range¹
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6,500 nm
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12,046 km
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Long Range Cruise Speed
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Mach 0.80
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459 ktas
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851 km/h
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Takeoff Distance²
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5,990 ft
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1,826 m
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Max Allowable Mach Number
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Mach 0.885
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Landing Distance³
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3,170 ft
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966 m
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Initial Cruise Altitude
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41,000 ft
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12,497 m
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Maximum Cruise Altitude
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51,000 ft
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15,545 m
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¹ Mach 0.80, 8 passengers, 4 crew, NBAA IFR reserves
² SL, ISA, MTOW
³ SL, ISA, MLW
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Aircraft Weights
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Maximum Takeoff Weight
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90,500 lb
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41,051 kg
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Maximum Landing Weight
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75,300 lb
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34,156 kg
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Maximum Zero Fuel Weight
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54,500 lb
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24,721 kg
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Basic Operating Weight¹
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48,000 lb
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21,773 kg
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Maximum Payload
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6,500 lb
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2,948 kg
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Payload with Maximum Fuel
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1,600 lb
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726 kg
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Maximum Fuel Weight
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41,300 lb
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18,734 kg
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Allowance for outfitting/operating items
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8,500 lb
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3,856 kg
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¹ including 4 crew
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Aircraft Design Standards
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Engines (2)
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BMW Rolls-Royce BR710
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Rated Takeoff Thrust ea.
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14,750 lb
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65.6 kN
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Maximum Passengers
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19
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Passengers¹
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13-15
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Cabin Pressure Differential
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10.17 psid, 6,000 ft cabin at 51K ft
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¹ Typical Outfitting
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Aircraft Interior
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Cabin Entry Door Dimensions
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36 in x 60 in
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91.4 cm x 152.4 cm
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Cabin Length
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50 ft 1 in
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15.3 m
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Cabin Height
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6 ft 2 in
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1.9 m
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Cabin Width
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7 ft 4 in
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2.2 m
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Cabin Volume
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1,669 cu ft
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47.3 cu m
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Baggage Compartment Vol.
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226 cu ft
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6.4 cu m
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Aircraft Exterior
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Length
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96 ft 5 in
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29.4 m
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Height
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25 ft 10 in
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7.9 m
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Wingspan
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93 ft 6 in
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28.5 m
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