C-37

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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