Accession Number:

AD0843171

Title:

Centaur Propellant Utilization Ratio Error Detector Assembly. Vibration Test Procedure.

Descriptive Note:

Corporate Author:

GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s):

Report Date:

1962-02-28

Pagination or Media Count:

9.0

Abstract:

The purpose was to specify requirements and procedures for testing and checkout of the Centaur ratio error detector assembly during vibration. Author

Subject Categories:

  • Liquid Rocket Propellants
  • Ground Support Systems and Facilities for Space Vehicles

Distribution Statement:

APPROVED FOR PUBLIC RELEASE