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gptkbp:instance_of
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gptkb:aircraft
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gptkbp:aircraft_operated
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gptkb:engine
turboprop aircraft
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gptkbp:avionics
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modernized for its time
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gptkbp:crew
|
2
1-2
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gptkbp:design
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gptkb:Grumman_Aerospace_Corporation
low-wing monoplane
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gptkbp:engine
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2
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gptkbp:engine_type
|
turboprop
Rolls-Royce Dart 510
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gptkbp:first_flight
|
gptkb:1958
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gptkbp:fuel_capacity
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1,200 liters
1,200 liters/hour
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|
gptkbp:historical_significance
|
first aircraft designed specifically for business use.
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|
https://www.w3.org/2000/01/rdf-schema#label
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Gulfstream I-SP
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gptkbp:interior_features
|
1.83 m
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|
gptkbp:landing_gear
|
tricycle gear
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gptkbp:length
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19.4 m
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gptkbp:manufacturer
|
gptkb:Gulfstream_Aerospace
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|
gptkbp:market_segment
|
business aviation
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gptkbp:max_speed
|
500 knots
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|
gptkbp:max_takeoff_weight
|
900 m
1,200 m
8,600 kg
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|
gptkbp:notable_features
|
pressurized cabin
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|
gptkbp:primary_user
|
private operators
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gptkbp:produced_by
|
approximately 200
|
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gptkbp:production_years
|
1958-1970
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|
gptkbp:range
|
1,500 nautical miles
1,800 miles
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gptkbp:retirement_year
|
gptkb:1970
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gptkbp:role
|
gptkb:engine
|
|
gptkbp:seating_capacity
|
8-10
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|
gptkbp:service_ceiling
|
25,000 feet
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|
gptkbp:services
|
gptkb:1960
|
|
gptkbp:successor
|
gptkb:Gulfstream_II
|
|
gptkbp:surface
|
elevators, ailerons, rudder
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gptkbp:variant
|
gptkb:Gulfstream_I
|
|
gptkbp:weight
|
5,500 kg
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|
gptkbp:width
|
2.08 m
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gptkbp:wing_area
|
60 m²
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gptkbp:wingspan
|
20.1 m
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gptkbp:bfsParent
|
gptkb:Gulfstream_I
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gptkbp:bfsLayer
|
4
|