• Rocket Engine, Liquid Fuel, Orbital Attitude Maneuvering System (OAMS), Gemini
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    Cylindrical, metallic, with canted 30 degree elliptical exhaust exit. Designed with this shaped nozzle to fit the contours of the Gemini spacecraft. Two propellant feed-in pipes jutting out from top of cylinder, in V-pattern, with smaller pipes attached. Nozzle, phenolic.

Created by

Smithsonian National Air and Space Museum

Date Created

07/08/2022

Source

Smithsonian National Air and Space Museum

Keywords

Engines; Gemini Program; Missions; Rockets; Space

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