Accession Number:

AD0843171

Title:

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

Personal Author(s):

Corporate Author:

GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Report Date:

1962-02-28

Abstract:

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

Pages:

0009

Descriptors:

Identifiers:

Subject Categories:

File Size:

0.00MB

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