Accession Number:

AD0861787

Title:

Propellant Residuals and Mixture Ratio for an F-2 Mission,

Descriptive Note:

Corporate Author:

GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s):

Report Date:

1962-09-28

Pagination or Media Count:

13.0

Abstract:

This study was made to determine the propellant residuals and mixture ratio deviation of the engines on Centaur F-2 if the mixture ratio control system operated at its upper or lower failure mode limits or at null throughout the flight. Author

Subject Categories:

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

Distribution Statement:

APPROVED FOR PUBLIC RELEASE