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