Lunar Instrument Carrier
Attitude Stabilization
ResearchPublished 1956
An estimate of the magnitudes of various attitude disturbances acting on a moon rocket. Such disturbances include initial misalignment, initial pitch and yaw rates, solar radiation torque, and the gravitational gradient of the earth. In addition, vehicle design restrictions are indicated.
Document Details
- Copyright: RAND Corporation
- Availability: Available
- Year: 1956
- Print Format: Paperback
- Paperback Pages: 25
- Paperback Price: $20.00
- Document Number: RM-1730
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Buchheim, Robert W., Lunar Instrument Carrier: Attitude Stabilization, RAND Corporation, RM-1730, 1956. As of September 24, 2024: https://www.rand.org/pubs/research_memoranda/RM1730.html
Buchheim, Robert W., Lunar Instrument Carrier: Attitude Stabilization. Santa Monica, CA: RAND Corporation, 1956. https://www.rand.org/pubs/research_memoranda/RM1730.html. Also available in print form.
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