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ST7-DRS: A Step Towards Drag-free and High-precision Formation ControlThe Space Technology 7 Disturbance Reduction System (ST7-DRS) is an in-space technology demonstration within NASA's New Millennium Program. ST7-DRS is designed to validate system-level technologies that are required for future gravity missions (including the planned LISA gravitational-wave observatory) and for future formation-flying interferometer missions (including the planned MAXIM black-hole imager). ST7-DRS is based around a freely-floating test mass contained within a spacecraft structure that will shield this test mass from all external forces (aside from gravity). The spacecraft position will be continuously controlled, such that the spacecraft, itself, will remain centered about this test mass, essentially flying in formation with it. Colloidal micro-thrusters will be used to control the spacecraft s position to within a few nanometers, over time scales of tens to thousands of seconds. In order to detect the residual acceleration noise on the main test mass, a second test mass will be flown alongside the first, within the same physical spacecraft structure. This test mass will serve as a cross-reference for the first, and will also be used as a reference for the spacecraft's attitude control. The spacecraft's attitude will be controlled to an accuracy of a few milli-arc-seconds, also utilizing the colloidal micro-thrusters. ST7-DRS will consist of an instrument package (containing the test masses) and a set of micro-thrusters, which will be attached to the European Space Agency s SMART-2 spacecraft, set to launch in November 2007.
Document ID
20040012862
Acquisition Source
Goddard Space Flight Center
Document Type
Conference Paper
Authors
Houghton, M.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Folkner, W.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Hanson, J.
(Stanford Univ. Stanford, CA, United States)
Hruby, V.
(Busek (J.) Co., Inc. Natick, MA, United States)
Date Acquired
August 21, 2013
Publication Date
January 1, 2003
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: 2004 IEEE Aerospace Conference: In-Space Technology Valdation Missions
Location: Big Sky, MT
Country: United States
Start Date: March 6, 2004
End Date: March 13, 2004
Sponsors: Institute of Electrical and Electronics Engineers
Distribution Limits
Public
Copyright
Other

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