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Space shuttle auxiliary propulsion system design study. phase c and e report: storable propellants, rcs/oms/apu integration study
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Perryman, D. C. Bruns, A. E. Wieland, D. L. Anglim, D. D. |
| Copyright Year | 1972 |
| Description | Auxiliary propulsion concepts for application to the space shuttle are compared. Both monopropellant and bipropellant earth storable reaction control systems were evaluated. The fundamental concepts evaluated were: (1) monopropellant and bipropellant systems installed integrally within the vehicle, (2) fuel systems installed modularly in nose and wing tip pods, and (3) fuel systems installed modularly in nose and fuselage pods. Numerous design variations within these three concepts were evaluated. The system design analysis and methods for implementing each of the concepts are reported. |
| File Size | 13644415 |
| Page Count | 390 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19730011105 |
| Archival Resource Key | ark:/13960/t9x10vr5m |
| Language | English |
| Publisher Date | 1972-12-29 |
| Access Restriction | Open |
| Subject Keyword | Propulsion Systems Fuel Systems Monopropellants Space Shuttles Liquid Rocket Propellants Systems Analysis Auxiliary Propulsion Propulsion System Configurations Spacecraft Configurations Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
