C-37
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The C-37 is a multi-purpose transport aircraft developed by the American firm Gulfstream Aerospace. It is based on the civilian Gulfstream V and represents a further evolution in the Gulfstream aircraft series, bearing similarities to the C-20H Gulfstream IV.
Development and Production
Serial production of the C-37 commenced on May 5, 1997. The aircraft entered service in July 1998.
Role and Program
This aircraft was developed under the U.S. Air Force VC-X program and serves as a complement to the C-32 aircraft.
Technical Specifications
| Modification | С-37А |
| Wingspan, m | 28.50 |
| Aircraft length, m | 29.40 |
| Aircraft height, m | 7.90 |
| Empty weight | 21773 |
| Maximum takeoff weight | 41051 |
| Internal fuel, l | 18734 |
| Engine type | 2 Turbofan engines BMW Rolls-Royce BR710 |
| Thrust, kN | 2 x 65.60 |
| Maximum speed, km/h | 941 |
| Cruising speed, km/h | 851 |
| Practical range, km | 12046 |
| Practical ceiling, m | 15545 |
| Crew, crew members | 2-3 |
| Payload | up to 19 passengers or 2948 kg of cargo |
Image and diagram gallery of the C-37
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American