Loading...
Please wait, while we are loading the content...
Experimental hydrogen-fluorine rocket performance at low pressures and high ratios
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1963 |
| Description | Hydrogen-fluorine performance at low combustion chamber pressures in rockets with high area ratio exhaust nozzles |
| File Size | 6333971 |
| Page Count | 32 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19660024035 |
| Archival Resource Key | ark:/13960/t3130md37 |
| Language | English |
| Publisher Date | 1963-09-01 |
| Access Restriction | Open |
| Subject Keyword | Rocket Engine Chamber Pressure Hydrogen Exhaust Nozzle Fluorine Combustion Chamber Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |