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Wear Testing of the HERMeS ThrusterThe Hall-Effect Rocket with Magnetic Shielding (HERMeS) thruster is being developed and tested at NASA GRC and NASA JPL through support of the Space Technology Mission Directorate (STMD) as primary propulsion for the Asteroid Rendezvous and Redirect Mission (ARRM). This thruster is advancing the state of the art of hall-effect thrusters (HETs) and is intended to serve as a precursor to higher power systems for human interplanetary exploration. The HERMeS Thruster Demonstration Unit One (TDU-1) has entered a 2000-hour wear test campaign at NASA GRC and has completed the first three of four test segments totaling 728 hours of operation. This is the first test of a NASA-designed magnetically shielded thruster to extend beyond 300 hours of continuous operation.
Document ID
20170003032
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Williams, George J.
(Ohio Aerospace Inst. Cleveland, OH, United States)
Gilland, James H.
(Ohio Aerospace Inst. Cleveland, OH, United States)
Peterson, Peter Y.
(Vantage Partners, LLC Cleveland, OH, United States)
Kamhawi, Hani
(NASA Glenn Research Center Cleveland, OH United States)
Huang, Wensheng
(NASA Glenn Research Center Cleveland, OH United States)
Ahern, Drew W.
(NASA Glenn Research Center Cleveland, OH United States)
Yim, John
(NASA Glenn Research Center Cleveland, OH United States)
Herman, Daniel A.
(NASA Glenn Research Center Cleveland, OH United States)
Hofer, Richard R.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Sekerak, Michael
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
April 6, 2017
Publication Date
July 1, 2016
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AIAA Paper 2016-5025
GRC-E-DAA-TN34124
Meeting Information
Meeting: AIAA/SAE/ASEE Joint Propulsion Conference
Location: Salt Lake City, UT
Country: United States
Start Date: July 25, 2016
End Date: July 27, 2016
Sponsors: Society of Automotive Engineers, Inc., American Society for Engineering Education (ASEE), American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 729200.06.03.05
CONTRACT_GRANT: NNG15CR66C
CONTRACT_GRANT: NNC12BA01B
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Thruster
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