Title:
Reusable Exploration Vehicle (REV): Orbital Space Tourism Concept

dc.contributor.author Clark, Ian G. en_US
dc.contributor.author Francis, Scott R. en_US
dc.contributor.author Otero, Richard E. en_US
dc.contributor.author Wells, Grant William en_US
dc.date.accessioned 2006-03-17T15:57:58Z
dc.date.available 2006-03-17T15:57:58Z
dc.date.issued 2005-05
dc.description 2005 RASC-AL Design Competition May 2005, Coco Beach, FL. en_US
dc.description.abstract On the heels of the recent success of the X-Prize, sub-orbital space tourism is nearly a reality. Though the requirements are significantly tougher, orbital space tourism is the next logical step. The Reusable Exploration Vehicle (REV) concept is an economically feasible design capable of making this next step. Centered around a lenticular lifting body, the REV concept relies on commercial launch vehicles to reduce DDT&E expenditures. Capable of ferrying five passengers and one crew member for three orbits, the REV is shown to be capable of keeping maximum debt exposure to less than $250M while attaining an IRR of 70% with an estimated market capture of 66%.
dc.format.extent 406364 bytes
dc.format.mimetype application/pdf
dc.identifier.uri http://hdl.handle.net/1853/8373
dc.language.iso en_US
dc.publisher Georgia Institute of Technology en_US
dc.relation.ispartofseries SSDL ;
dc.subject Space tourism
dc.subject Reusable exploration vehicles
dc.subject Lenticular bodies
dc.subject Design requirements
dc.subject Revolutionary Aerospace Systems Concept - Academic Liason (RASC-AL)
dc.subject Space commercialization
dc.title Reusable Exploration Vehicle (REV): Orbital Space Tourism Concept en_US
dc.type Text
dc.type.genre Paper
dspace.entity.type Publication
local.contributor.corporatename Space Systems Design Laboratory (SSDL)
local.contributor.corporatename Daniel Guggenheim School of Aerospace Engineering
local.contributor.corporatename Daniel Guggenheim School of Aerospace Engineering
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relation.isOrgUnitOfPublication a348b767-ea7e-4789-af1f-1f1d5925fb65
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