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SIM trajectory designSIM (Space Interferometry Mission) is a mission scheduled to launch in 2010 and will be the first spacecraft to use interferometry to measure the positions of stars to within 1 micro-arcsecond - a degree of precision never to before achieve. The flight hardware required to achieve this level of precision is very sensitive to its external environment, which places a number of challenging constraints on the trajectory design. This paper discusses the various trajectory options that were considered.
Document ID
20060043750
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
Authors
Johnson, Wyatt R.
Date Acquired
August 23, 2013
Publication Date
August 16, 2004
Subject Category
Astrodynamics
Meeting Information
Meeting: AIAA/AAS Astrodynamics Specialist Conference
Location: Providence, RI
Country: United States
Start Date: August 16, 2004
End Date: August 19, 2004
Distribution Limits
Public
Copyright
Other
Keywords
Titan Mission
ballute
aerocapture

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