This page no longer updated from 31 October 2001. Latest version can be found at G-1

G-1 -

Credit: Boeing / Rocketdyne. 11,799 bytes. 166 x 286 pixels.

Manufacturer Name: G-1. Government Designation: Nomad. Designer: Rocketdyne. Developed in: 1958. Application: Atlas upper stage. . Propellants: LF2/Hydrazine Thrust(vac): 5,450 kgf. Thrust(vac): 53.50 kN. Isp: 357 sec. Status: Developed 1960's. Comments: Engine developed for replacement of Agena upper stage in late 1950's. Not flown due to toxicity of propellants. NOMAD Upper Stage System. Pressure-fed.
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Last update 12 March 2001.
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© Mark Wade, 2001 .