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Flow system startup of a full-scale simulated nuclear rocket engine
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1965 |
| Description | Performance of liquid hydrogen flow system during startup transient of nuclear rocket in full scale simulated engine system |
| File Size | 1890426 |
| Page Count | 15 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19650025799 |
| Archival Resource Key | ark:/13960/t8pc7qt1k |
| Language | English |
| Publisher Date | 1965-01-01 |
| Access Restriction | Open |
| Subject Keyword | Flow Characteristics Fuel Flow Nuclear Rocket Liquid Hydrogen Rocket Engine 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 |