Title:
System Architecture Tools and Assumptions
System Architecture Tools and Assumptions
dc.contributor.author | Reeves, David M. | en_US |
dc.contributor.author | Scher, Michael D. | en_US |
dc.contributor.author | Shidner, Jeremy | en_US |
dc.contributor.author | Thomas, Paige D. | en_US |
dc.contributor.author | Bucher, Dean | en_US |
dc.contributor.author | Roithmayr, Carlos | en_US |
dc.contributor.corporatename | National Institute of Aerospace | en_US |
dc.contributor.corporatename | Georgia Institute of Technology. School of Aerospace Engineering | en_US |
dc.contributor.corporatename | Georgia Institute of Technology. Space Systems Design Lab | en_US |
dc.date.accessioned | 2006-01-24T15:20:26Z | en_US |
dc.date.accessioned | 2006-03-03T21:11:42Z | |
dc.date.available | 2006-01-24T15:20:26Z | en_US |
dc.date.available | 2006-03-03T21:11:42Z | |
dc.date.issued | 2005-11-09 | en_US |
dc.description | This conference features the work of authors from: Georgia Tech’s Space Systems Design Lab, Aerospace Systems Design Lab, School of Aerospace Engineering, Georgia Tech Research Institute; NASA’s Jet Propulsion Laboratory, Marshall Space Flight Center, Goddard Space Flight Center, Langley Research Center; and other aerospace industry and academic institutions | en_US |
dc.description.abstract | Discussion of various system architecture tools and assumptions available to modify existing architectures for new requirements and mission objectives. This study started from proven Apollo concept and adjusted it for new requirements and mission objectives. New technologies were included to decrease size and cost. A crew size trade study is presented to demonstrate how mass size, propulsion size, and trajectory are calculated for an unmanned and up to four man crew in lunar exploration missions | en_US |
dc.description.sponsorship | AIAA Space Systems Technical Committee ; AIAA Space Transportation Systems Technical Committee ; Space Technology Advanced Research Center | en_US |
dc.format.extent | 6780180 bytes | en_US |
dc.format.extent | 1905 bytes | |
dc.format.extent | 6780180 bytes | |
dc.format.mimetype | application/pdf | |
dc.format.mimetype | text/plain | |
dc.format.mimetype | application/pdf | |
dc.identifier.uri | http://hdl.handle.net/1853/8039 | |
dc.language.iso | en_US | en_US |
dc.publisher | Georgia Institute of Technology | en_US |
dc.relation.ispartofseries | SSEC05 Session E;GT-SSEC.E.5 | en_US |
dc.subject | Aerospace architecture tools | en_US |
dc.subject | Crew size trade studies | en_US |
dc.subject | Mass sizing tools | en_US |
dc.subject | Mission objectives | en_US |
dc.subject | Mission requirements | en_US |
dc.subject | Simulated trajectories | en_US |
dc.subject | Apollo mission architecture | en_US |
dc.subject | Space propulsion sizing | en_US |
dc.title | System Architecture Tools and Assumptions | en_US |
dc.type | Text | |
dc.type.genre | Presentation | |
dspace.entity.type | Publication | |
local.contributor.corporatename | Aerospace Systems Design Laboratory (ASDL) | |
local.relation.ispartofseries | Space Systems Engineering Conference | |
relation.isOrgUnitOfPublication | a8736075-ffb0-4c28-aa40-2160181ead8c | |
relation.isSeriesOfPublication | a55c7ee7-6ea7-4115-bdc9-63faecf45826 |