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Thrust Stand for Vertically Oriented Electric Propulsion Performance EvaluationA variation of a hanging pendulum thrust stand capable of measuring the performance of an electric thruster operating in the vertical orientation is presented. The vertical orientation of the thruster dictates that the thruster must be horizontally offset from the pendulum pivot arm, necessitating the use of a counterweight system to provide a neutrally-stable system. Motion of the pendulum arm is transferred through a balance mechanism to a secondary arm on which deflection is measured. A non-contact light-based transducer is used to measure displacement of the secondary beam. The members experience very little friction, rotating on twisting torsional pivots with oscillatory motion attenuated by a passive, eddy current damper. Displacement is calibrated using an in situ thrust calibration system. Thermal management and self-leveling systems are incorporated to mitigate thermal and mechanical drifts. Gravitational restoring force and torsional spring constants associated with flexure pivots provide restoring moments. An analysis of the design indicates that the thrust measurement range spans roughly four decades, with the stand capable of measuring thrust up to 12 N for a 200 kg thruster and up to approximately 800 mN for a 10 kg thruster. Data obtained from calibration tests performed using a 26.8 lbm simulated thruster indicated a resolution of 1 mN on 100 mN-level thrusts, while those tests conducted on 200 lbm thruster yielded a resolution of roughly 2.5 micro at thrust levels of 0.5 N and greater.
Document ID
20100033281
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Moeller, Trevor
(Tennessee Univ. Space Inst. Tullahoma, TN, United States)
Polzin, Kurt A.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 25, 2013
Publication Date
July 25, 2010
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
M10-0918
Report Number: M10-0918
Meeting Information
Meeting: 46th AIAA/ASME/SAE/ASEE Joint Propulsin Conference
Location: Nashville, TN
Country: United States
Start Date: July 25, 2010
End Date: July 28, 2010
Sponsors: American Society of Mechanical Engineers, American Society for Electrical Engineers, American Inst. of Aeronautics and Astronautics, Society of Automotive Engineers, Inc.
Funding Number(s)
CONTRACT_GRANT: FA9109-06-D-0001/0001
CONTRACT_GRANT: F40 600-DO-D-0001/0024
Distribution Limits
Public
Copyright
Public Use Permitted.
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