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):

• Shimizu, T.
• Luster, J.
• Berlin, E.

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:

• (*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 Systems and Facilities for Space Vehicles

Distribution Statement:

APPROVED FOR PUBLIC RELEASE