Accession Number:

AD0842957

Title:

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

Descriptive Note:

Corporate Author:

GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s):

Report Date:

1961-03-01

Pagination or Media Count:

50.0

Abstract:

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

Subject Categories:

  • Electrical and Electronic Equipment
  • Rocket Engines
  • Ground Support Systems and Facilities for Space Vehicles

Distribution Statement:

APPROVED FOR PUBLIC RELEASE