Citation
Wiley, Robert Freeland (1973) On the Use of Fixed Attitude Propulsive Arcs for Transfer Between Neighboring Coplanar Keplerian Orbits. Engineer's thesis, California Institute of Technology. doi:10.7907/456S-YS44. https://resolver.caltech.edu/CaltechTHESIS:09232010-115331989
Abstract
The question of whether or not a coplanar, fixed attitude, constant acceleration burn in a central force field can result in a post-burn orbit that does not intersect the pre-burn orbit was investigated for small changes in the orbit. This was done by developing a criterion for separation between coplanar elliptical orbits, solving the linearized equations of motion given in reference 1 for a coplanar, fixed attitude, constant acceleration burn, and evaluating the criterion. Regions in which an initial alignment of the acceleration vector may be chosen to result in orbital separation at some point in the burn and the alignments of the acceleration vector to do this were found numerically. However, it appears that the distances between the separated orbits and the time over which the orbits separate for a particular alignment are too small to make the phenomenon of much practical use for small orbital changes.
Item Type: | Thesis (Engineer's thesis) |
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Subject Keywords: | (Aeronautical Engineering) |
Degree Grantor: | California Institute of Technology |
Division: | Engineering and Applied Science |
Major Option: | Aeronautics |
Thesis Availability: | Public (worldwide access) |
Research Advisor(s): |
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Group: | GALCIT |
Thesis Committee: |
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Defense Date: | 1 January 1973 |
Record Number: | CaltechTHESIS:09232010-115331989 |
Persistent URL: | https://resolver.caltech.edu/CaltechTHESIS:09232010-115331989 |
DOI: | 10.7907/456S-YS44 |
Default Usage Policy: | No commercial reproduction, distribution, display or performance rights in this work are provided. |
ID Code: | 6042 |
Collection: | CaltechTHESIS |
Deposited By: | Dan Anguka |
Deposited On: | 23 Sep 2010 21:22 |
Last Modified: | 16 Jul 2024 00:19 |
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