• DocumentCode
    2906950
  • Title

    Innovative approach enabled the retirement of TDRS-1 compliant with NASA orbital debris requirements

  • Author

    Zaleski, Ronald ; Mirczak, Walter ; Staich, Stephen ; Caverly, Richard ; Smith, Eric ; Teti, Nicholas ; Vaught, W. Lynn ; Olney, Dave

  • Author_Institution
    NASA Goddard Space Flight Center, Greenbelt, MD, USA
  • fYear
    2011
  • fDate
    5-12 March 2011
  • Firstpage
    1
  • Lastpage
    22
  • Abstract
    The first Tracking and Data Relay Satellite (TDRS-1) was deactivated on June 27th 2010 following more than 26 years of operation. The end-of-mission (EOM) operations were developed to address the stringent requirements of NPR 8715.6: NASA Procedural Requirements for Limiting Orbital Debris, which consists of three key items: 1) removal from the geosynchronous arc; 2) depletion of the remaining propellant; and 3) passivation of all sources of energy storage or generation. The EOM approach minimized risks while accomplishing these goals. Raising TDRS-1 over 350 km above geosynchronous was accomplished via proven station change operations. Depleting propellant was the most challenging task, requiring over 20 hours of thruster on-time accumulated within schedule, orbit, and spacecraft subsystem constraints. The attitude configuration and operational procedures, including the unique final passivation method, were thoroughly analyzed and simulated prior to the start of operations. The complete EOM campaign lasted 21 days. The TDRS-1 EOM campaign demonstrated that pre-NPR 8715.6 satellite designs can be made to comply1 and that lessons learned could be applied to other satellite designs. The significant TDRS-1 effort demonstrates a commitment by NASA to responsible orbital debris management in compliance with international standards.
  • Keywords
    artificial satellites; propellants; space debris; EOM operation; NASA orbital debris requirements; NASA procedural requirements for limiting orbital debris; TDRS-1 compliant; end-of-mission operation; geosynchronous arc; orbital debris management; passivation method; propellant; spacecraft subsystem; thruster; tracking and data relay satellite; Attitude control; Fuels; NASA; Orbits; Propulsion; Space debris; 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.2011.5747304
  • Filename
    5747304