The purpose of this test is to determine that the ground and airborne pressurization systems will function properly to pressurize the fuel and L02 tanks before and during firing of the missile. The test will consist of conducting a 'blow-down' operation by pressurizing the fuel and L02 tank simulation ullage tanks in the manner which the missile fuel and L02 tank will be pressurized to and during firing. (Author)
Checkout and Validation, Ground/Airborne Pneumatic Systems
1958
19 pages
Report
Keine Angabe
Englisch
Missile Technology , Rocket Propellants , Surface to surface missiles , Propellant tanks , Pressurization , Performance(Engineering) , Simulation , Helium , Pneumatic devices , Checkout procedures , Valves , Oscillation , Compressors , Control panels , Test methods , Ullage , Xsm-65b missiles , Xsm-65c missiles
Onboard versus ground checkout systems
AIAA | 1971
|Advanced ground support checkout systems.
NTRS | 1972
|Developments in on-board and ground checkout systems
AIAA | 1970
|