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The Development of NASA's Low Thrust Trajectory Tool SetHighly efficient electric propulsion systems can enable interesting classes of missions; unfortunately, they provide only a limited amount of thrust. Low-thrust (LT) trajectories are much more difficult to design than impulsive-type (chemical propulsion) trajectories. Previous low-thrust (LT) trajectory optimization software was often difficult to use, often had difficulties converging, and was somewhat limited in the types of missions it could support. A new state-of-the-art suite (toolbox) of low-thrust (LT) tools along with improved algorithms and methods was developed by NASA's MSFC, JPL, JSC, and GRC to address the needs of our customers to help foster technology development in the areas of advanced LT propulsion systems, and to facilitate generation of similar results by different analysts.
Document ID
20070002635
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Sims, Jon
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Artis, Gwen
Kos, Larry
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 24, 2013
Publication Date
January 1, 2006
Subject Category
Spacecraft Propulsion And Power
Meeting Information
Meeting: Division for Planetary Sciences Meeting
Location: Pasadena, CA
Country: United States
Start Date: October 8, 2006
End Date: October 13, 2006
Distribution Limits
Public
Copyright
Public Use Permitted.
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