The Effect of Direct Solar Radiation on the Attitude of the Skynet Spacecraft.
Abstract
Analytical expressions are derived for the forces and torques acting on a spin stabilized cylindrical satellite due to direct solar radiation. These expressions are then used to determine the effects of direct solar radiation on the attitude and orbit of the SKYNET spacecraft, and a comparison is made with the observed behaviour of the spacecraft. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Feb 11, 1972
- Accession Number
- AD0747694
Entities
People
- G. J. Davison
- R. H. Merson
Organizations
- Royal Aircraft Establishment