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Evaluation of 7.8-inch-throat-diameter inserts and a unique cooling concept in a storable- propellant rocket engine
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1969 |
| Description | Nozzle insert evaluation and gas cooling concept in storable liquid propellant rocket engine |
| File Size | 24675360 |
| Page Count | 35 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19690010428 |
| Archival Resource Key | ark:/13960/t14n3xp7h |
| Language | English |
| Publisher Date | 1969-03-01 |
| Access Restriction | Open |
| Subject Keyword | Propulsion Systems 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 |