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Analytical investigation of three turbopump feed systems suitable for high-pressure hydrogen-oxygen rocket-engine applications
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1965 |
| Description | Turbopump feed systems for high pressure hydrogen- oxygen rocket engines |
| File Size | 1442626 |
| Page Count | 31 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19650021359 |
| Archival Resource Key | ark:/13960/t1mh2bx6q |
| Language | English |
| Publisher Date | 1965-08-01 |
| Access Restriction | Open |
| Subject Keyword | Turbopump Hydrox Engine Feed System 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 |