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Experimental performance of a 5000-pound- thrust rocket chamber using a 20-percent- fluorine - 80-percent-oxygen mixture with rp-1
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1957 |
| Description | Increased performance of rocket engine using fluorine-oxygen mixture with RP-1 fuel |
| File Size | 16988486 |
| Page Count | 26 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19660030239 |
| Archival Resource Key | ark:/13960/t6sz11c4w |
| Language | English |
| Publisher Date | 1957-04-24 |
| Access Restriction | Open |
| Subject Keyword | Fluorine-liquid Oxygen /flox/ Rocket Engine 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 |