Accession Number : AD0831511

Title :   MSTS TEST REPORT, TEST 95-402-A1-S1.

Corporate Author : GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Report Date : 12 MAY 1959

Pagination or Media Count : 40

Abstract : 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)

Descriptors :   *PROPELLANT TANKS), (*SURFACE TO SURFACE MISSILES, (*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.

Subject Categories : Surface-launched Guided Missiles
      Liquid Rocket Propellants

Distribution Statement : APPROVED FOR PUBLIC RELEASE