The objective of the test was to determine the minimum pressure to actuate the vernier fuel tank and oxidizer tank pressurizing shuttle valves.
'E' Series Vernier Pneumatic Control Manifold
1960
7 pages
Report
No indication
English
Manufacturing Processes & Materials Handling , Rocket Propellants , Missile Technology , Vernier rocket engines , Valves , Propellant control , Performance(Engineering) , Pneumatic devices , Solenoids , Leakage(Fluid) , Pressurization , Propellant transfer , Liquid rocket oxidizers , Surface to surface missiles , Shuttle valves , Atlas , Xsm-65e missiles
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