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Dynamics during thrust maneuvers of flexible spinning satellites with axial and radial booms
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Longman, R. W. Fedor, J. V. |
| Copyright Year | 1986 |
| Description | The dynamic response to operational maneuvers of spinning symmetric spacecraft with radial and axial booms was analyzed as part of the prelaunch dynamic analysis of the ISEE-3 spacecraft placed in a halo orbit around an Earth-Sun libration point, and later renamed ICE when it was directed to fly-by comet Giacobini-Zinner. The results presented use simple spacecraft models, and frequently give predictions that are good and easily obtained when the results from using a general purpose multibody dynamics program were very time consuming to obtain. Deployment of radial booms, spin-up after partial deployment, stationkeeping, and trajectory changes are analyzed. The latter two can involve both axial thrusting and pulsed radial thrusting once per revolution. |
| File Size | 533067 |
| Page Count | 6 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19870015922 |
| Archival Resource Key | ark:/13960/t3sv2gb1w |
| Language | English |
| Publisher Date | 1986-12-01 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Design, Testing And Performance Spacecraft Maneuvers Flexible Spacecraft Booms Equipment Thrust Vector Control Deployment Vibration Mode Astrodynamics International Sun Earth Explorer 3 Spacecraft Models Spin Stabilization Trajectory Analysis Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
