The object of this test was to evaluate the performance of the airborne regulators during a MA-3 engine start using nitrogen gas in the PCU. (Author)
'E' Regulator GN2 Start Test (GN2 Pcu Evaluation for 'E' Series Missiles
1960
44 pages
Report
No indication
English
Rocket Engines & Motors , Laboratory & Test Facility Design & Operation , Liquid propellant rocket engines , Propellant control , Ignition , Surface to surface missiles , Performance(Engineering) , Nitrogen , Liquefied gases , Test methods , Pressurization , Atlas , Evaluation , Ma-3 propulsion systems , Ullage , Xsm-65e missiles
Engineering Index Backfile | 1957
|Springer Verlag | 2016
|Flight Summary Report on Series D Atlas Missiles
NTIS | 1961