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
Descriptors:
Subject Categories:
- Liquid Rocket Propellants
- Ground Support Systems and Facilities for Space Vehicles