Accession Number:

AD0844521

Title:

Propellant Tanking Overflow Tube,

Descriptive Note:

Corporate Author:

GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s):

Report Date:

1961-06-20

Pagination or Media Count:

11.0

Abstract:

The objective of the test was to utilize the fuel standpipe and the oxidizer standpipe overflow tubes to accurately indicate and preserve the 100 station level during propellant loading. Author

Subject Categories:

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

Distribution Statement:

APPROVED FOR PUBLIC RELEASE