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Experimental performance of a hydrogen- fluorine rocket engine at several chamber pressures and exhaust-nozzle expansion area ratios
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1960 |
| Description | Experimental performance of hydrogen-fluorine rocket engine at several chamber pressures and exhaust-nozzle expansion area ratios |
| File Size | 6057940 |
| Page Count | 37 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19660024058 |
| Archival Resource Key | ark:/13960/t58d4n71s |
| Language | English |
| Publisher Date | 1960-10-01 |
| Access Restriction | Open |
| Subject Keyword | Nozzle Expansion Hydrogen Fuel Fluorine Liquid Propellant Rocket Engine Chamber Pressure 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 |