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Ssme alternate turbopump development program: design verification specification for high-pressure fuel turbopump
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1989 |
| Description | The design and verification requirements are defined which are appropriate to hardware at the detail, subassembly, component, and engine levels and to correlate these requirements to the development demonstrations which provides verification that design objectives are achieved. The high pressure fuel turbopump requirements verification matrix provides correlation between design requirements and the tests required to verify that the requirement have been met. |
| File Size | 4176308 |
| Page Count | 88 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19900000717 |
| Archival Resource Key | ark:/13960/t2n63fg8z |
| Language | English |
| Publisher Date | 1989-04-21 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Propulsion And Power Turbine Pumps Performance Tests Specifications Design Analysis Vibration Tests Fuel Pumps High Pressure Structural Analysis 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 |
