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Performance Characterization of the Air Force Transformational Satellite 12 kW Hall ThrusterThe STMD GCD ISP project is tasked with developing, maturing, and testing enabling human exploration propulsion requirements and potential designs for advanced high-energy, in-space propulsion systems to support deep-space human exploration and reduce travel time between Earth's orbit and future destinations for human activity. High-power Hall propulsion systems have been identified as enabling technologies and have been the focus of the activities at NASA Glenn-In-house effort to evaluate performance and interrogate operation of NASA designed and manufactured Hall thrusters. Evaluate existing high TRL EP devices that may be suitable for implementation in SEP TDM.
Document ID
20140010771
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Kamhawi, Hani
(NASA Glenn Research Center Cleveland, OH United States)
Haag, Thomas W.
(NASA Glenn Research Center Cleveland, OH United States)
Smith, Timothy
(NASA Glenn Research Center Cleveland, OH United States)
Herman, Daniel
(NASA Glenn Research Center Cleveland, OH United States)
Huang, Wensheng
(NASA Glenn Research Center Cleveland, OH United States)
Shastry, Rohit
(NASA Glenn Research Center Cleveland, OH United States)
Peterson, Peter
(Aerojet Redmond, WA, United States)
Mathers, Alex
(Aerojet Redmond, WA, United States)
Date Acquired
August 18, 2014
Publication Date
April 29, 2013
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
GRC-E-DAA-TN12405
Meeting Information
Meeting: Spacecraft Propulsion
Location: Colorado, Springs, CO
Country: United States
Start Date: April 29, 2013
End Date: May 2, 2013
Sponsors: Department of the Army, Department of the Navy, NASA Headquarters, Department of the Air Force
Funding Number(s)
WBS: WBS 272725.04.02.02.02.03
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Propulsion
Electric Propulsion
Hall Thrusters
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