DocumentCode :
1934871
Title :
Game changing: NASA´s space launch system and science mission design
Author :
Creech, S.D.
Author_Institution :
Space Launch Syst. Program, Nat. Aeronaut. & Space Adm., Marshall Space Flight Center, AL, USA
fYear :
2013
fDate :
2-9 March 2013
Firstpage :
1
Lastpage :
13
Abstract :
NASA´s Marshall Space Flight Center (MSFC) is directing efforts to build the Space Launch System (SLS), a heavy-lift rocket that will carry the Orion Multi-Purpose Crew Vehicle (MPCV) and other important payloads far beyond Earth orbit (BEO). Its evolvable architecture will allow NASA to begin with Moon fly-bys and then go on to transport humans or robots to distant places such as asteroids and Mars. Designed to simplify spacecraft complexity, the SLS rocket will provide improved mass margins and radiation mitigation, and reduced mission durations. These capabilities offer attractive advantages for ambitious missions such as a Mars sample return, by reducing infrastructure requirements, cost, and schedule. For example, if an evolved expendable launch vehicle (EELV) were used for a proposed mission to investigate the Saturn system, a complicated trajectory would be required - with several gravity-assist planetary fly-bys - to achieve the necessary outbound velocity. The SLS rocket, using significantly higher characteristic energy (C3) energies, can more quickly and effectively take the mission directly to its destination, reducing trip time and cost. As this paper will report, the SLS rocket will launch payloads of unprecedented mass and volume, such as “monolithic” telescopes and in-space infrastructure. Thanks to its ability to co-manifest large payloads, it also can accomplish complex missions in fewer launches. Future analyses will include reviews of alternate mission concepts and detailed evaluations of SLS figures of merit, helping the new rocket revolutionize science mission planning and design for years to come.
Keywords :
Earth orbit; Mars; Saturn; astronomical telescopes; rocket engines; space vehicles; BEO; EELV; MSFC; Mars sample return; Moon fly-bys; NASA marshall space flight center; NASA space launch system; Orion multipurpose crew vehicle; SLS rocket; Saturn system; asteroids; beyond Earth orbit; cost reduction; evolved expendable launch vehicle; gravity-assist planetary fly-bys; heavy-lift rocket; in-space infrastructure; infrastructure requirements; mass margins; mission duration reduction; monolithic telescope; radiation mitigation; science mission design; spacecraft complexity; trip time reduction; NASA; Payloads; Rockets; Space missions; Space vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference, 2013 IEEE
Conference_Location :
Big Sky, MT
ISSN :
1095-323X
Print_ISBN :
978-1-4673-1812-9
Type :
conf
DOI :
10.1109/AERO.2013.6496921
Filename :
6496921
Link To Document :
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