Computer program was written to evaluate and define optimum design parameters of low pressure auxiliary propulsion system. APS will provide attitude and translational control of space shuttle vehicles. Program evaluates subsystem design parameters such as engine chamber pressure, mixture ratio, expansion ratio, and subsystem component weight and size.
Propulsion sizing program
1972-10-01
Miscellaneous
No indication
English
Propulsion System Sizing Methodology and Tool
AIAA | 2007
|SPT sizing for integrated propulsion systems
AIAA | 1996
|SPT Sizing for Integrated Propulsion Missions
British Library Conference Proceedings | 1996
|Propulsion system sizing for servicing spacecrafts
IEEE | 2008
|PRELIMINARY SIZING CORRELATIONS FOR UAVS´PROPULSION SYSTEM
TIBKAT | 2019
|