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Cold-air performance evaluation of scale model oxidizer pump-drive turbine for the m-1 hydrogen-oxygen rocket engine. ii - overall two-stage performance
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1966 |
| Description | Cold flow test of pump drive turbines for M-1 rocket engine |
| File Size | 1683016 |
| Page Count | 35 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19660010314 |
| Archival Resource Key | ark:/13960/t4tj37z4c |
| Language | English |
| Publisher Date | 1966-03-01 |
| Access Restriction | Open |
| Subject Keyword | M-1 Rocket Engine Turbine Cold Flow Test 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 |