From Wikipedia, the free encyclopedia
The Gulfstream II is an American 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. A modified version of the C-11, called the Shuttle Training Aircraft (STA), mimics the cockpit configuration and flight characteristics of the Space Shuttle and is used by NASA as a training airplane for practice shuttle approaches (referred to as "dives").
[edit] Operators
[edit] Military operators
Morocco
Oman
Venezuela
United States
[edit] Non-military operators
Panama
- Part of the presidential fleet, 1 aircraft
[edit] Specifications
Data from The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985), 1985, Orbis Publishing, Page 2053
General characteristics
- Crew: 2
- Length: 79 ft 11 in (24.36 m)
- Wingspan: 77 ft 10 in (23.72 m)
- Height: 24 ft 6 in (7.47 m)
- Wing area: 934.6 ft² (86.82 m²)
- Empty weight: 39100 lb (17725 kg)
- Gross weight: 66200 lb (30935 kg)
- Powerplant: 2 × Two Rolls-Royce Spey 511-8 turbofan, 11,400 lbf ( kN) each
Performance
- Maximum speed: Mach 0.85
- Range: 4088 miles (6579 km)
- Service ceiling: 45000 ft (13715 m)
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[edit] See also
Related development
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United States tri-service transport designations post-1962 |
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