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Space shuttle auxiliary propulsion system design study. phase a report: requirements definition
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Orton, G. F. Schweickert, T. F. |
| Copyright Year | 1972 |
| Description | The analyses and rationale used to develop requirements for the oxygen-hydrogen auxiliary propulsion systems to be used with the space shuttle are presented. The requirements apply to a fully reusable space shuttle vehicle system using internal, reusable main engine propellant tanks in both the orbiter and booster stages. Requirements of principal interest are engine thrust, number of engines, maximum system thrust, total impulse, and total impulse expenditure history. |
| File Size | 2353842 |
| Page Count | 63 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19730011101 |
| Archival Resource Key | ark:/13960/t3sv2bv9t |
| Language | English |
| Publisher Date | 1972-02-15 |
| Access Restriction | Open |
| Subject Keyword | Propulsion Systems Equipment Specifications Space Shuttles Systems Analysis Auxiliary Propulsion Propulsion System Configurations Requirements Gaseous Rocket Propellants 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 |
