Accession Number : AD0842957

Title :   Design Proofing Test Report for Centaur Propellant Utilization Ratio Error Detector.

Corporate Author : GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s) : Kaleta, G. J.

Report Date : 01 MAR 1961

Pagination or Media Count : 50

Abstract : The objective of the test was to conduct all design proofing tests on the Centaur propellant utilization ratio error detector. (Author)

Descriptors :   *DETECTORS), (*LAUNCH VEHICLES, LIQUID PROPELLANT ROCKET ENGINES), (*PROPELLANT CONTROL, PERFORMANCE(ENGINEERING), HUMIDITY, AMPLIFIERS, DEMODULATORS, CIRCUITS, MANOMETERS, ELECTRICAL RESISTANCE, CAPACITANCE, ELECTRIC SWITCHES, VIBRATION, ACCELERATION, VOLTAGE, THERMAL STABILITY.

Subject Categories : Electrical and Electronic Equipment
      Rocket Engines
      Ground Support Sys & Facil For Space Vehicles

Distribution Statement : APPROVED FOR PUBLIC RELEASE