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Additional Mission Applications for NASA's 13.3-kW Ion Propulsion SystemNASA's Space Technology Mission Directorate has been recently developing critical technologies for high-power solar electric propulsion (SEP), including large deployable solar array structures and high-power electric propulsion components. An ion propulsion system based on these developments has been considered for many SEP technology demonstration missions, including the Asteroid Redirect Robotic Mission (ARRM) concept. These studies and the highpower SEP technology developments have generated excitement within NASA about the use of the ARRM ion propulsion system design for other types of potential missions. One application of interest is for Mars missions, especially with the types of orbiters now under consideration for flights in the early 2020's to replace the aging Mars Reconnaissance Orbiter. High-power SEP can deliver large payloads to Mars with many additional capabilities, including large orbital plane changes and roundtrip missions, compared to chemically-propelled spacecraft. Another application for high-power SEP is for exo-planet observation missions, where a large starshade spacecraft would need to be repositioned with respect to its companion telescope relatively frequently and rapidly. SEP is an enabling technology for the ambitious science goals of these types of missions. This paper will discuss the benefits of high-power SEP for these concepts based on the STMD technologies now under development.
Document ID
20170007091
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
Authors
Snyder, John Steven
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Manzella, David
(NASA Glenn Research Center Cleveland, OH, United States)
Lisman, Doug
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Lock, Robert E.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Nicholas, Austin
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Woolley, Ryan
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 1, 2017
Publication Date
March 5, 2016
Subject Category
Spacecraft Design, Testing And Performance
Launch Vehicles And Launch Operations
Lunar And Planetary Science And Exploration
Meeting Information
Meeting: Annual IEEE Aerospace Conference 2016
Location: Big Sky, MT
Country: United States
Start Date: March 3, 2016
End Date: March 10, 2016
Sponsors: Institute of Electrical and Electronics Engineers
Distribution Limits
Public
Copyright
Other
Keywords
Space Technology Mission Directorate
solar electric propulsion

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