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Nozzle and cavity wall cooling limitations on specific impulse of a gas-core nuclear rocket
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1971 |
| Description | Nozzle and cavity wall cooling limitations on specific impusle of gas-core nuclear rocket engine |
| File Size | 1601691 |
| Page Count | 10 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19710026319 |
| Archival Resource Key | ark:/13960/t18m22f9h |
| Language | English |
| Publisher Date | 1971-01-01 |
| Access Restriction | Open |
| Subject Keyword | Nuclear Engineering Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |