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Propulsion system needs
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Gunn, Stanley |
| Copyright Year | 1991 |
| Description | The needs of the designer of a solid core nuclear rocket engine are discussed. Some of the topics covered include: (1) a flight thrust module/feed system module assembly; (2) a nuclear thermal rocket (NTR), expander cycle, dual T/P; (3) turbopump operating conditions; (4) typical system parameters; (5) growth capability composite fuel elements; (6) a NTR radiation cooled nozzle extension; (7) a NFS-3B Feed System; and (8) a NTR Integrated Pneumatic-Fluidics Control System. |
| File Size | 645476 |
| Page Count | 14 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19920001894 |
| Archival Resource Key | ark:/13960/t42r8r55w |
| Language | English |
| Publisher Date | 1991-01-01 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Propulsion And Power Rocket Nozzles Nozzle Design Turbine Pumps Nuclear Propulsion Pneumatic Control Feed Systems Reactor Cores Rocket Engine Design Propulsion System Configurations Nuclear Rocket Engines Spacecraft Propulsion Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
