Published June 30, 1971
| Version v1
Report
Restricted
Thermionic spacecraft design study, 120 kw nuclear electric propulsion system. Volume 2. External fuel reactor spacecraft design. Final report
Description
no abstract available
Availability note (English)
MF available from INIS under the Report Number.
Files
Restricted
The record is publicly accessible, but files are restricted to users with access.
Additional details
Publishing Information
- Imprint Pagination
- 101 p.
- Report number
- N--71-38533
INIS
- Country of Publication
- United States
- Country of Input or Organization
- United States
- INIS RN
- 3032122
- Subject category
- S21: SPECIFIC NUCLEAR REACTORS AND ASSOCIATED PLANTS;
- Descriptors DEI
- NUCLEAR FUELS; PERFORMANCE; PROPULSION; REACTORS; SPACE VEHICLES; THERMIONIC CONVERTERS; URANIUM 233
- Descriptors DEC
- ALPHA DECAY RADIOISOTOPES; DIRECT ENERGY CONVERTERS; EVEN-ODD NUCLEI; FUELS; HEAVY NUCLEI; ISOTOPES; NUCLEI; RADIOISOTOPES; REACTOR COMPONENTS; REACTOR MATERIALS; URANIUM ISOTOPES; YEARS LIVING RADIOISOTOPES
Optional Information
- Notes
- For Jet Propulsion Lab., Pasadena, Calif.
- Secondary number(s)
- NASA-CR--122927; GESP--648(Vol.2).