Interplanetary charged particle models (1974). NASA space vehicle design criteria (environment)
Description
The design of space vehicles for operation in interplanetary space is given, based on descriptions of solar wind, solar particle events, and galactic cosmic rays. A state-of-the-art review is presented and design criteria are developed from experiment findings aboard interplanetary and high-altitude earth-orbiting spacecraft. Solar cells were found to be particularly sensitive. Solar protons may also impact the reliability of electric propulsion systems and spacecraft surfaces, as well as causing interference, detector saturation, and spurious signals. Galactic cosmic-ray impact can lead to similar electronic failure and interference, and may register in photographic films and other emulsions. It was concluded that solar wind electron measurements might result from differential charging when shadowed portions of the spacecraft acquired a negative charge from electron impact
Availability note (English)
MF available from INIS under the Report Number.
Files
Additional details
Publishing Information
- Imprint Pagination
- 47 p.
- Report number
- N--75-24607
INIS
- Country of Publication
- United States
- Country of Input or Organization
- United States
- INIS RN
- 8307500
- Subject category
- S46: INSTRUMENTATION RELATED TO NUCLEAR SCIENCE AND TECHNOLOGY; S79: ASTROPHYSICS, COSMOLOGY AND ASTRONOMY;
- Descriptors DEI
- CHARGED PARTICLES; COSMIC RADIATION; ELECTRONIC EQUIPMENT; ELECTRONS; ELEMENTARY PARTICLES; ENERGETIC SOLAR PARTICLES; FAILURES; FERMIONS; INTERFERENCE; INTERPLANETARY SPACE; LEPTONS; PROTONS; RADIATION EFFECTS; RADIATIONS; RELIABILITY; SOLAR CELLS; SOLAR RADIATION; SOLAR WIND; SPACE VEHICLES; SPECIFICATIONS; STELLAR RADIATION
- Descriptors DEC
- BARYONS; CATIONS; DIRECT ENERGY CONVERTERS; HADRONS; HYDROGEN IONS; HYDROGEN IONS 1 PLUS; IONIZING RADIATIONS; IONS; NUCLEONS; SOLAR ACTIVITY; SPACE
Optional Information
- Notes
- Available from NTIS. $3.75.
- Secondary number(s)
- NASA-SP--8118.