Contents: Demonstrate the structural integrity of the missile and missile ducting; Develop a procedure for loading HE-LN2 aboard the missile that is compatible with IOC requirements; Demonstrate the structural integrity of the airborne helium system at high loading rates; Evaluate the Convair propellant loading control system in properly controlling propellant levels in the missile tanks during loading operations; and Develop an integrated propellant loading cycle employing sequences generally compatible with IOC concepts. (Author)
Msts Test Report, Test 95-402-A1-S1
1959
40 pages
Report
Keine Angabe
Englisch
Rocket Propellants , Missile Technology , Surface to surface missiles , Propellant tanks , Propellant transfer , Checkout procedures , Structural properties , Pressurization , Liquid level control , Ground support equipment , Control panels , Indicator lights , Flowmeters , Valves , Errors , Pressure , Temperature , Sequences(Mathematics) , Pipes , Control systems , Drainage , Heat transfer , Walls , Liquid rocket oxidizers , Propellant control , Atlas
Online Contents | 1995
MSTS prototype for Arctic waters
Engineering Index Backfile | 1955