Share Email Print
cover

Proceedings Paper

Assessing the challenges to a geosynchronous space tug system
Format Member Price Non-Member Price
PDF $14.40 $18.00

Paper Abstract

A space tug vehicle is designed to rendezvous and dock with a space object; make an assessment of its current position, orientation, and operational status; and then either stabilize the object in its current orbit or move the object to a new location with subsequent release. A subset of on-orbit servicing, space tug missions in the geosynchronous belt include stationkeeping of satellites which have lost attitude control and repositioning of satellites. Repositioning of spacecraft may be desirable as a means to rescue satellites launched into incorrect orbits, for the retirement of satellites into “graveyard” orbits, and for on-demand maneuvers that support flexible mission requirements. This paper aims to unify the political, legal, operational, and financial aspects of the space tug concept and highlight the challenges that stand in the way of an operational space tug vehicle. U.S. Space Transportation Policy is reviewed, and a space tug operation is recognized as an enabler of emerging national space transportation requirements. Customary international and United States laws are explored as potential constraining forces on future tug missions. A concept of operations in geosynchronous orbit, including parking orbit selection and approach strategies, is analyzed with emphasis placed on safety and reliability. Potential financing models and the issue of insurance for space tugs are discussed and identified as the principal challenges facing implementation of a space tug system. This paper offers a positive forecast for the future of on-orbit servicing and endorses continued government support for proof-of-concept missions.

Paper Details

Date Published: 19 May 2005
PDF: 11 pages
Proc. SPIE 5799, Modeling, Simulation, and Verification of Space-based Systems II, (19 May 2005); doi: 10.1117/12.603975
Show Author Affiliations
Matthew G. Richards, Massachusetts Institute of Technology (United States)
Philip N. Springmann, Massachusetts Institute of Technology (United States)
Michelle E. McVey, Massachusetts Institute of Technology (United States)


Published in SPIE Proceedings Vol. 5799:
Modeling, Simulation, and Verification of Space-based Systems II
Pejmun Motaghedi, Editor(s)

© SPIE. Terms of Use
Back to Top