• DocumentCode
    2910214
  • Title

    Simple, robust cryogenic propellant depot for near term applications

  • Author

    McLean, Christopher ; Pitchford, Brian ; Mustafi, Shuvo ; Wollen, Mark ; Walls, Laurie ; Schmidt, Jeff

  • Author_Institution
    Ball Aerosp. & Technol. Corp., Boulder, CO, USA
  • fYear
    2011
  • fDate
    5-12 March 2011
  • Firstpage
    1
  • Lastpage
    24
  • Abstract
    The ability to refuel cryogenic propulsion stages on-orbit provides an innovative paradigm shift for space transportation supporting National Aeronautics and Space Administration´s (NASA) Exploration program as well as deep space robotic, national security and commercial missions. Refueling enables large beyond low Earth orbit (LEO) missions without requiring super heavy lift vehicles that must continuously grow to support increasing mission demands as America´s exploration transitions from early Lagrange point missions to near Earth objects (NEO), the lunar surface and eventually Mars. Earth-to-orbit launch can be optimized to provide competitive, cost-effective solutions that allow sustained exploration.
  • Keywords
    aerospace instrumentation; cryogenics; propellants; NASA Exploration program; cryogenic propulsion; low Earth orbit missions; robust cryogenic propellant depot; space transportation; Cryogenics; Earth; Low earth orbit satellites; NASA; Propulsion; Space vehicles;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2011 IEEE
  • Conference_Location
    Big Sky, MT
  • ISSN
    1095-323X
  • Print_ISBN
    978-1-4244-7350-2
  • Type

    conf

  • DOI
    10.1109/AERO.2011.5747488
  • Filename
    5747488