• DocumentCode
    2792114
  • Title

    SHERPA: A Flexible & Responsive Small Satellite Transport Vehicle

  • Author

    Fram, Lt Bryan ; Sauter, Lt Luke ; Buckley, Steven ; Summers, Bob ; Rogers, Aaron

  • Author_Institution
    Kirtland Air Force Base, Albuquerque, NM
  • fYear
    2005
  • fDate
    5-12 March 2005
  • Firstpage
    1
  • Lastpage
    8
  • Abstract
    SHERPA1,2, the Shuttle Expendable Rocket for Payload Augmentation, is a highly capable propulsive satellite. The SHERPA is currently approaching a PDR level design. The SHERPA can perform a wide range of missions including orbit transfers, small satellite maneuvers, space situational awareness missions, and serve as a platform for experiments. The SHERPA has three versions: The Mark I, is a propulsion unit, the Mark II is a standalone propulsive satellite, and the Mark III, a self contained long-duration propulsive satellite. Each version can support either an electric or chemical propulsion module. The SHERPA integrates several Air Force Research Laboratory developed technologies into one unique package. The SHERPA can also fulfil a number of other mission needs as a low cost satellite bus for the DoD Space Test Program
  • Keywords
    aerospace propulsion; artificial satellites; space research; Mark I propulsion unit; Mark II standalone propulsive satellite; Mark III self contained long-duration propulsive satellite; SHERPA; orbit transfers; payload augmentation; satellite maneuvers; shuttle expendable rocket; small satellite transport vehicle; space situational awareness missions; Chemicals; Laboratories; Payloads; Propulsion; Rockets; Satellites; Space missions; Space shuttles; Space technology; Vehicles;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2005 IEEE
  • Conference_Location
    Big Sky, MT
  • Print_ISBN
    0-7803-8870-4
  • Type

    conf

  • DOI
    10.1109/AERO.2005.1559583
  • Filename
    1559583