This page no longer updated from 31 October 2001. Latest version can be found at G-38 Navaho Booster

Navaho G-38 Engine
Navaho G-38 Engine - Navaho G-38 3 Engine Cluster

47,245 bytes. 306 x 436 pixels.

Gross Mass: 76,870 kg. Empty Mass: 16,780 kg. Thrust (vac): 208,854 kgf. Isp: 282 sec. Burn time: 90 sec. Propellants: Lox/Kerosene Isp(sl): 248 sec. Diameter: 2.4 m. Span: 2.4 m. Length: 27.4 m. Country: USA. No Engines: 3. LR-83-NA-1 Status: Cancelled 1957. Other designations: XB-64A, XSM-64A. Comments: Burns out at altitude 21,600 m, Mach 3. Empty Mass estimated.
Back to Index
Last update 12 March 2001.
Definitions of Technical Terms.
Contact Mark Wade with any corrections or comments.
Conditions for use of drawings, pictures, or other materials from this site..
© Mark Wade, 2001 .