Computer based satellite design

Computer based satellite design

Approved for public release; distribution is unlimited === A computer program to design geosynchronous spacecraft has been developed. The program consists of four separate but interrelated executable computer programs. The programs are compiled to run on an dos based personal computer. the source...

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Main Author: Lashbrook, David L.
Other Authors: Agrawal, Brij N.
Language:en_US
Published: Monterey, California. Naval Postgraduate School 2012
Online Access:http://hdl.handle.net/10945/23582
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spelling ndltd-nps.edu-oai-calhoun.nps.edu-10945-235822015-08-06T16:03:10Z Computer based satellite design Lashbrook, David L. Agrawal, Brij N. Wight, Randy L. Naval Postgraduate School Department of Aeronautics and Astronautics Approved for public release; distribution is unlimited A computer program to design geosynchronous spacecraft has been developed. The program consists of four separate but interrelated executable computer programs. The programs are compiled to run on an dos based personal computer. the source computer code is written in DoD mandated Ada programming language. The thesis presents the design techniques and design equations used in the program. Detailed analysis is performed in the following areas for both dual-spin and three axis stabilized spacecraft configuration: Mass propellant budget and mass summary; Battery cell and solar cell requirements for a payload power requirement; Passive thermal control requirements. Thesis includes a users manual Appendix A, and the source code for the computer programs in Appendix B. 2012-11-29T16:13:48Z 2012-11-29T16:13:48Z 1992-06 Thesis http://hdl.handle.net/10945/23582 en_US This publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. As such, it is in the public domain, and under the provisions of Title 17, United States Code, Section 105, it may not be copyrighted. Monterey, California. Naval Postgraduate School
collection NDLTD
language en_US
sources NDLTD
description Approved for public release; distribution is unlimited === A computer program to design geosynchronous spacecraft has been developed. The program consists of four separate but interrelated executable computer programs. The programs are compiled to run on an dos based personal computer. the source computer code is written in DoD mandated Ada programming language. The thesis presents the design techniques and design equations used in the program. Detailed analysis is performed in the following areas for both dual-spin and three axis stabilized spacecraft configuration: Mass propellant budget and mass summary; Battery cell and solar cell requirements for a payload power requirement; Passive thermal control requirements. Thesis includes a users manual Appendix A, and the source code for the computer programs in Appendix B.
author2 Agrawal, Brij N.
author_facet Agrawal, Brij N.
Lashbrook, David L.
author Lashbrook, David L.
spellingShingle Lashbrook, David L.
Computer based satellite design
author_sort Lashbrook, David L.
title Computer based satellite design
title_short Computer based satellite design
title_full Computer based satellite design
title_fullStr Computer based satellite design
title_full_unstemmed Computer based satellite design
title_sort computer based satellite design
publisher Monterey, California. Naval Postgraduate School
publishDate 2012
url http://hdl.handle.net/10945/23582
work_keys_str_mv AT lashbrookdavidl computerbasedsatellitedesign
_version_ 1716816366106836992

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