Mission Design Considerations for the Tundra Constellation
The geostationary orbit belt has become highly populated with communication satellites, making frequency allocations more challenging to obtain. An innovative solution to this problem may be provided by the recently proposed Tundra orbit constellation. The Tundra constellation uses three or more spa...
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ftmissouriunivst:oai:scholarsmine.mst.edu:mec_aereng_facwork-4073 2023-06-11T04:17:23+02:00 Mission Design Considerations for the Tundra Constellation Bruno, M. J. Pernicka, Henry J. 2002-08-08T07:00:00Z https://scholarsmine.mst.edu/mec_aereng_facwork/2566 https://doi.org/10.2514/6.2002-4634 unknown Scholars' Mine https://scholarsmine.mst.edu/mec_aereng_facwork/2566 doi:10.2514/6.2002-4634 https://doi.org/10.2514/6.2002-4634 © 2002 American Institute of Aeronautics and Astronautics (AIAA), All rights reserved. Mechanical and Aerospace Engineering Faculty Research & Creative Works Aerospace Engineering Mechanical Engineering text 2002 ftmissouriunivst https://doi.org/10.2514/6.2002-4634 2023-05-06T22:28:24Z The geostationary orbit belt has become highly populated with communication satellites, making frequency allocations more challenging to obtain. An innovative solution to this problem may be provided by the recently proposed Tundra orbit constellation. The Tundra constellation uses three or more spacecraft in inclined geosynchronous orbits. The needed terrestrial coverage is obtained by proper orientation of each orbit relative to the constellation and by proper phasing of each satellite within its orbit. The nominal orbit design for the constellation should minimize any negative perturbation effects in order to provide affordable stationkeeping costs. This study describes an initial examination of the Tundra constellation given basic constraints. Mission design elements are first considered followed by a discussion of stationkeeping issues. Perturbation effects from thirdbody and geopotential sources are quantified and used to select nominal orbits that will provide the needed coverage and that can be maintained within reasonable fuel budgets. © 2002 by the author(s). Text Tundra Missouri University of Science and Technology (Missouri S&T): Scholars' Mine AIAA/AAS Astrodynamics Specialist Conference and Exhibit |
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Missouri University of Science and Technology (Missouri S&T): Scholars' Mine |
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ftmissouriunivst |
language |
unknown |
topic |
Aerospace Engineering Mechanical Engineering |
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Aerospace Engineering Mechanical Engineering Bruno, M. J. Pernicka, Henry J. Mission Design Considerations for the Tundra Constellation |
topic_facet |
Aerospace Engineering Mechanical Engineering |
description |
The geostationary orbit belt has become highly populated with communication satellites, making frequency allocations more challenging to obtain. An innovative solution to this problem may be provided by the recently proposed Tundra orbit constellation. The Tundra constellation uses three or more spacecraft in inclined geosynchronous orbits. The needed terrestrial coverage is obtained by proper orientation of each orbit relative to the constellation and by proper phasing of each satellite within its orbit. The nominal orbit design for the constellation should minimize any negative perturbation effects in order to provide affordable stationkeeping costs. This study describes an initial examination of the Tundra constellation given basic constraints. Mission design elements are first considered followed by a discussion of stationkeeping issues. Perturbation effects from thirdbody and geopotential sources are quantified and used to select nominal orbits that will provide the needed coverage and that can be maintained within reasonable fuel budgets. © 2002 by the author(s). |
format |
Text |
author |
Bruno, M. J. Pernicka, Henry J. |
author_facet |
Bruno, M. J. Pernicka, Henry J. |
author_sort |
Bruno, M. J. |
title |
Mission Design Considerations for the Tundra Constellation |
title_short |
Mission Design Considerations for the Tundra Constellation |
title_full |
Mission Design Considerations for the Tundra Constellation |
title_fullStr |
Mission Design Considerations for the Tundra Constellation |
title_full_unstemmed |
Mission Design Considerations for the Tundra Constellation |
title_sort |
mission design considerations for the tundra constellation |
publisher |
Scholars' Mine |
publishDate |
2002 |
url |
https://scholarsmine.mst.edu/mec_aereng_facwork/2566 https://doi.org/10.2514/6.2002-4634 |
genre |
Tundra |
genre_facet |
Tundra |
op_source |
Mechanical and Aerospace Engineering Faculty Research & Creative Works |
op_relation |
https://scholarsmine.mst.edu/mec_aereng_facwork/2566 doi:10.2514/6.2002-4634 https://doi.org/10.2514/6.2002-4634 |
op_rights |
© 2002 American Institute of Aeronautics and Astronautics (AIAA), All rights reserved. |
op_doi |
https://doi.org/10.2514/6.2002-4634 |
container_title |
AIAA/AAS Astrodynamics Specialist Conference and Exhibit |
_version_ |
1768376509648601088 |