Accession Number : AD0861787

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

Corporate Author : GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CA

Personal Author(s) : Shimizu, T. ; Luster, J. ; Berlin, E.

Report Date : 28 SEP 1962

Pagination or Media Count : 13

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)

Descriptors :   (*LAUNCH VEHICLES, PROPELLANT CONTROL), (*FUEL CONSUMPTION, PREDICTIONS), LIQUID PROPELLANT ROCKET ENGINES, LIQUID ROCKET PROPELLANTS, PROPELLANT TANKS, MIXTURES, BULKHEADS, HEAT TRANSFER, AERODYNAMIC HEATING, OPTIMIZATION.

Subject Categories : Liquid Rocket Propellants
      Ground Support Sys & Facil For Space Vehicles

Distribution Statement : APPROVED FOR PUBLIC RELEASE