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Assessment of Spacecraft Systems Integration Using the Electric Propulsion Interactions Code (EPIC)SAIC is currently developing the Electric Propulsion Interactions Code 'EPIC', an interactive computer tool that allows the construction of a 3-D spacecraft model, and the assessment of interactions between its subsystems and the plume from an electric thruster. EPIC unites different computer tools to address the complexity associated with the interaction processes. This paper describes the overall architecture and capability of EPIC including the physics and algorithms that comprise its various components. Results from selected modeling efforts of different spacecraft-thruster systems are also presented.
Document ID
20020090844
Acquisition Source
Marshall Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Mikellides, Ioannis G.
(Science Applications International Corp. San Diego, CA United States)
Kuharski, Robert A.
(Science Applications International Corp. San Diego, CA United States)
Mandell, Myron J.
(Science Applications International Corp. San Diego, CA United States)
Gardner, Barbara M.
(Science Applications International Corp. San Diego, CA United States)
Kauffman, William J.
Date Acquired
September 7, 2013
Publication Date
July 1, 2002
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AIAA Paper 2002-3667
Report Number: AIAA Paper 2002-3667
Meeting Information
Meeting: 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference
Location: Indianapolis, IN
Country: United States
Start Date: July 7, 2002
End Date: July 10, 2002
Sponsors: American Society of Mechanical Engineers, American Society for Electrical Engineers, Society of Automotive Engineers, Inc., American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NAS8-02028
Distribution Limits
Public
Copyright
Public Use Permitted.
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