Accession Number:

AD0861403

Title:

Design Proof Test Report for the Centaur Zero 'G' Vent System GD/A Part No. 55-80021-3 Spec. No. 55-08129 Vendor - GD/A,

Descriptive Note:

Corporate Author:

GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s):

Report Date:

1962-06-22

Pagination or Media Count:

90.0

Abstract:

The purpose of the test was to prove the design of the Zero G Vent System for the liquid hydrogen fuel tank of the Centaur Space Vehicle. Author

Subject Categories:

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

Distribution Statement:

APPROVED FOR PUBLIC RELEASE