• DocumentCode
    3514864
  • Title

    Descent Assisted Split Habitat Lunar Lander Concept

  • Author

    Mazanek, Daniel D. ; Goodliff, Kandyce E. ; Cornelius, David M.

  • Author_Institution
    Langley Res. Center, Nat. Aeronaut. & Space Adm. (NASA), Hampton, VA
  • fYear
    2008
  • fDate
    1-8 March 2008
  • Firstpage
    1
  • Lastpage
    16
  • Abstract
    The descent assisted split habitat (DASH) lunar lander concept utilizes a disposable braking stage for descent and a minimally sized pressurized volume for crew transport to and from the lunar surface. The lander can also be configured to perform autonomous cargo missions. Although a braking-stage approach represents a significantly different operational concept compared with a traditional two-stage lander, the DASH lander offers many important benefits. These benefits include improved crew egress/ingress and large-cargo unloading; excellent surface visibility during landing; elimination of the need for deep-throttling descent engines; potentially reduced plume-surface interactions and lower vertical touchdown velocity; and reduced lander gross mass through efficient mass staging and volume segmentation. This paper documents the conceptual study on various aspects of the design, including development of sortie and outpost lander configurations and a mission concept of operations; the initial descent trajectory design; the initial spacecraft sizing estimates and subsystem design; and the identification of technology needs.
  • Keywords
    Moon; space vehicles; DASH lander; autonomous cargo missions; braking-stage approach; crew transport; descent assisted split habitat lunar lander; efficient mass staging; large-cargo unloading; lunar surface; minimally sized pressurized volume; outpost lander configurations; surface visibility; volume segmentation; Biographies; Engines; Humans; Moon; NASA; Payloads; Propulsion; Risk analysis; Space technology; Space vehicles;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2008 IEEE
  • Conference_Location
    Big Sky, MT
  • ISSN
    1095-323X
  • Print_ISBN
    978-1-4244-1487-1
  • Electronic_ISBN
    1095-323X
  • Type

    conf

  • DOI
    10.1109/AERO.2008.4526498
  • Filename
    4526498