Grumman Gulfstream II
From Wikipedia, the free encyclopedia
Gulfstream II | |
---|---|
A USCG Gulfstream II, 1969 | |
Type | Business jet |
Manufacturer | Grumman/Gulfstream Aerospace |
Developed from | Grumman Gulfstream I |
Variants | Gulfstream III |
The Gulfstream II is a large twin engine business jet built by Gulfstream Aerospace, and its US military designation is C-11 Gulfstream II. It has been succeeded by the C-20 Gulfstream III.
[edit] Military Operators
[edit] Specifications
- Length: 79.11 ft (24.1 m)
- Height: 24.6 ft (7.5 m)
- Wing span: 77.1 ft (23.5 m)
- Crew: 2
- Passenger: 19 maximum, 12 normal
- Speed: 459 mph
- Ceiling: 45,000 ft
- Cruise altitude: 39,000 ft
- Rate of climb: 4,350 ft/min
- Max weight: 65,000 lb (29,545 kg)
- Max payload: 5,456 lb (2,480 kg)
- Engine: Two Rolls-Royce Spey 511-8 @ 11,400 lb (5181 kg) each
[edit] Related content
Related development
Designation sequence
Related lists
- List of active United States military aircraft
Timeline of aviation
Aircraft · Aircraft manufacturers · Aircraft engines · Aircraft engine manufacturers · Airports · Airlines
Air forces · Aircraft weapons · Missiles · Unmanned aerial vehicles (UAVs) · Experimental aircraft
Notable military accidents and incidents · Notable airline accidents and incidents · Famous aviation-related deaths
Flight airspeed record · Flight distance record · Flight altitude record · Flight endurance record · Most produced aircraft