Accession Number:

AD0861341

Title:

Orifice Sizing and Component Evaluation for a Programmed LOX Tank Pressure on the Atlas/Agena Booster,

Descriptive Note:

Corporate Author:

GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s):

Report Date:

1962-09-19

Pagination or Media Count:

35.0

Abstract:

The objective of the test was to evaluate the performance of the components and the plumbing configuration required to program the LOX tank pressure needed during the flight of the AtlasAgena booster. Author

Subject Categories:

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

Distribution Statement:

APPROVED FOR PUBLIC RELEASE