G-1

G-1
Credit - Boeing / Rocketdyne

Manufacturer Name: G-1. Government Designation: Nomad. Designer: Rocketdyne. Developed in: 1958. Application: Atlas upper stage. Propellants: LF2/Hydrazine. Thrust(vac): 53.500 kN (12,027 lbf). Isp: 357 sec. Country: USA. Status: Developed 1960's.

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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