Spacecraft Design Project High Temperature Superconducting Infrared Imaging Satellite
dc.contributor.advisor | Agrawal, Brij | |
dc.contributor.author | Angus, Bill | |
dc.contributor.author | Covelli, Jeff | |
dc.contributor.author | Davinic, Nick | |
dc.contributor.author | Hailey, Jeff | |
dc.contributor.author | Jones, Evan | |
dc.contributor.author | Ortiz, Vince | |
dc.contributor.author | Racine, John | |
dc.contributor.author | Satterwhite, Doug | |
dc.contributor.author | Spriesterbach, Tom | |
dc.contributor.author | Sorensen, Dennis | |
dc.contributor.author | Sortun, Chris | |
dc.contributor.author | Vaughan, Rob | |
dc.contributor.author | Yi, Chon | |
dc.date | Fall 1989 | |
dc.date.accessioned | 2016-10-14T18:35:46Z | |
dc.date.available | 2016-10-14T18:35:46Z | |
dc.date.issued | 1991-12-18 | |
dc.identifier.uri | http://hdl.handle.net/10945/50293 | |
dc.description | NASA-CR-192036 | en_US |
dc.description | AE4871 Advance Spacecraft Design | |
dc.description | The 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.extent | 285 p. | en_US |
dc.language.iso | en_US | en_US |
dc.rights | This 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.title | Spacecraft Design Project High Temperature Superconducting Infrared Imaging Satellite | en_US |
dc.type | Report | en_US |