Statements (108)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:aircraft_operated |
gptkb:aircraft
gptkb:Gulfstream_family |
| gptkbp:capacity |
8 to 14 passengers
|
| gptkbp:certification |
gptkb:Certification
|
| gptkbp:competitors |
gptkb:Dassault_Falcon
gptkb:Bombardier_Challenger gptkb:Cessna_Citation |
| gptkbp:crew |
2 pilots
|
| gptkbp:design |
gptkb:Grumman_Aerospace_Corporation
low-wing business aviation |
| gptkbp:engine |
Pratt & Whitney Canada J T15 D
|
| gptkbp:engine_type |
twin-engine
|
| gptkbp:features |
high performance
modular design advanced avionics advanced safety features high-performance engines large windows swept wings quiet operation luxurious interior winglets reliable performance high thrust-to-weight ratio customizable interiors highly efficient engines high altitude performance pressurized cabin quiet cabin environment state-of-the-art navigation systems easy maintenance access fuel-efficient design retractable landing gear advanced wing design spacious cabin layout high-speed cruise capability multiple cabin configurations advanced materials used in construction long-range capability low drag design advanced aerodynamic design galley and lavatory facilities enhanced stability and control |
| gptkbp:first_flight |
gptkb:1966
|
| gptkbp:first_released |
gptkb:1967
|
| gptkbp:fuel_capacity |
14,000 lb
22,000 lb |
| gptkbp:height |
25 ft 5 in
|
| gptkbp:historical_significance |
pioneered business jet travel
influenced future designs in aviation set standards for luxury jets |
| https://www.w3.org/2000/01/rdf-schema#label |
Gulfstream II
|
| gptkbp:influenced |
subsequent Gulfstream models
|
| gptkbp:interior_features |
luxurious
|
| gptkbp:introduced |
gptkb:1966
gptkb:1967 |
| gptkbp:involved_units |
250
|
| gptkbp:landing_gear |
tricycle gear
|
| gptkbp:length |
88 ft 7 in
88 ft 3 in |
| gptkbp:manufacturer |
gptkb:Gulfstream_Aerospace
|
| gptkbp:market |
business aviation
|
| gptkbp:market_segment |
business jet market
|
| gptkbp:max_speed |
Mach 0.85
450 knots 600 mph |
| gptkbp:max_takeoff_weight |
60,000 lb
38,600 lb |
| gptkbp:modifications |
various upgrades available
|
| gptkbp:notable_features |
advanced avionics
high-speed cruise capability large cabin |
| gptkbp:notable_users |
gptkb:U._S._government
gptkb:celebrities government agencies corporate executives private individuals airlines for charter services |
| gptkbp:number_built |
250
|
| gptkbp:operational_history |
used for cargo transport
used for VIP transport used for air ambulance services used by governments and corporations |
| gptkbp:power_output |
Rolls-Royce Spey engines
|
| gptkbp:production_years |
1966-1986
1966 to 1970 1966 to 1980 |
| gptkbp:range |
3,800 nautical miles
3,400 nautical miles 3,600 nautical miles |
| gptkbp:retirement_year |
still in service with some operators
|
| gptkbp:role |
corporate transport
|
| gptkbp:safety_record |
generally safe
|
| gptkbp:seating_capacity |
8 to 12 passengers
|
| gptkbp:service_ceiling |
45,000 feet
45,000 ft |
| gptkbp:speed |
550 mph
Mach 0.80 |
| gptkbp:successor |
gptkb:Gulfstream_III
|
| gptkbp:type |
Business jet
|
| gptkbp:weight |
30,000 lb
|
| gptkbp:wing_area |
1,200 sq ft
|
| gptkbp:wingspan |
78 ft 9 in
78 ft 6 in |
| gptkbp:bfsParent |
gptkb:Gulfstream_I
|
| gptkbp:bfsLayer |
4
|