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Thruster Placement Issues and Possible Mitigation Methods for the ST-7 Disturbance Reduction SystemThe Space Technology-7 Disturbance Reduction System is being designed to demonstrate the ability to shield a test mass from non-gravitational forces. In order to meet this goal, two advanced technologies will be employed: a highly sensitive Gravitational Reference Sensor and micro-Newton thrusters. ST-7 is limited to two clusters of four thrusters, which are sufficient to provide control for 6 degrees of freedom, but the overall effectiveness of the baseline configuration is limited by the noise on the measurement signals and the thrust outputs, the disturbance force caused by solar radiation pressure, and the performance of the individual thrusters. This paper presents and discusses these issues in greater detail along with possible mitigation methods.
Document ID
20040082156
Acquisition Source
Goddard Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Hsu, O.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Markley, L.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Houghton, M.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Maghami, P.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2004
Subject Category
Spacecraft Propulsion And Power
Meeting Information
Meeting: Flight Dynamics Symposium
Location: Greenbelt, MD
Country: United States
Start Date: October 29, 2003
End Date: October 30, 2003
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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