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dc.contributor.advisorAgrawal, Brij
dc.contributor.authorAngus, Bill
dc.contributor.authorCovelli, Jeff
dc.contributor.authorDavinic, Nick
dc.contributor.authorHailey, Jeff
dc.contributor.authorJones, Evan
dc.contributor.authorOrtiz, Vince
dc.contributor.authorRacine, John
dc.contributor.authorSatterwhite, Doug
dc.contributor.authorSpriesterbach, Tom
dc.contributor.authorSorensen, Dennis
dc.contributor.authorSortun, Chris
dc.contributor.authorVaughan, Rob
dc.contributor.authorYi, Chon
dc.dateFall 1989
dc.date.accessioned2016-10-14T18:35:46Z
dc.date.available2016-10-14T18:35:46Z
dc.date.issued1991-12-18
dc.identifier.urihttp://hdl.handle.net/10945/50293
dc.descriptionNASA-CR-192036en_US
dc.descriptionAE4871 Advance Spacecraft Design
dc.descriptionThe High Temperature Super Conductor Infrared Imaging Satellite (HTSCIRIS) is designed to perform the space based infrared imaging and surveillance mission and is depicted in Figure 1.1. The design of the satellite follows the 'black box' approach. The payload is a stand alone unit, with the spacecraft bus designed to meet the requirements of the payload as listed in the statement of work presented in appendix A.
dc.format.extent285 p.en_US
dc.language.isoen_USen_US
dc.rightsThis publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. Copyright protection is not available for this work in the United States.en_US
dc.titleSpacecraft Design Project High Temperature Superconducting Infrared Imaging Satelliteen_US
dc.typeReporten_US


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