• 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