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
Link To Document