Accession Number:

AD0861780

Title:

Centaur A/P System Test (TSTS) (Structural),

Descriptive Note:

Corporate Author:

GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s):

Report Date:

1961-08-22

Pagination or Media Count:

34.0

Abstract:

The object of this test was to determine the magnitude and direction of deflections and spring constants of the Centaur engine mounts and upper actuator attach points when subjected to operational loads. Author

Subject Categories:

  • Couplers, Fasteners and Joints
  • Mechanics
  • Liquid Propellant Rocket Engines
  • Ground Support Systems and Facilities for Space Vehicles

Distribution Statement:

APPROVED FOR PUBLIC RELEASE