ORBITAL TESTING OF SNAP SYSTEMS
Journal Article
·
· Astronaut. Aerospace Eng.
OSTI ID:4661726
Objectives to be accomplished in orbital testing of Snap-2 and Snap-10A are outlined. The ability of vehicle components and subsystems to survive in the radiation environment, mechanical, thermal, and electrical interface problems unique to the utilization of nuclear power, and radiological safety precautions and procedures to be established in the orbital testing of Snap systems are discussed. (C.E.S.)
- Research Organization:
- Air Force Systems Command, Los Angeles
- NSA Number:
- NSA-17-035225
- OSTI ID:
- 4661726
- Journal Information:
- Astronaut. Aerospace Eng., Journal Name: Astronaut. Aerospace Eng. Vol. Vol: 1: No. 4
- Country of Publication:
- Country unknown/Code not available
- Language:
- English
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Related Subjects
COSMIC RADIATION
ELECTRICITY
MACHINE PARTS
MECHANICS
NESDPS Office of Nuclear Energy Space and Defense Power Systems
ORBITS
POWER
RADIATION EFFECTS
RADIATION PROTECTION
REACTORS
SAFETY
SNAP-10 SERIES
SNAP-2 SERIES
SPACE APPLICATIONS AND TECHNOLOGY
SPACE FLIGHT
SPACE VEHICLES
STANDARDS
TEMPERATURE
TESTING
ELECTRICITY
MACHINE PARTS
MECHANICS
NESDPS Office of Nuclear Energy Space and Defense Power Systems
ORBITS
POWER
RADIATION EFFECTS
RADIATION PROTECTION
REACTORS
SAFETY
SNAP-10 SERIES
SNAP-2 SERIES
SPACE APPLICATIONS AND TECHNOLOGY
SPACE FLIGHT
SPACE VEHICLES
STANDARDS
TEMPERATURE
TESTING