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/HydrazineThrust(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.