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Dawn Ion Propulsion System - Initial Checkout After LaunchThe first 80 days after launch of the Dawn mission were dedicated to the checkout of the spacecraft with a major emphasis on the ion propulsion system. All three ion thrusters, all three thruster-gimbal assemblies, both power processor units, both digital interface and control units, and the entire xenon feed system were completely checked out and every component was found to be in good health. Direct thrust measurements agreed well with preflight expected values for all three thrusters over the entire throttle range. Thruster electrical operating parameters and power processor units efficiencies also agreed well with preflight expected values based on acceptance test data. Two of the three ion thrusters were fully checked out within 30 days after launch. Checkout of all three thrusters was completed 64 days after launch. Deterministic thrusting with the IPS began on December 17, 2007.
Document ID
20150014772
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
Authors
Brophy, John R.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Garner, Charles E.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Mikes, Steven
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 3, 2015
Publication Date
July 21, 2008
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AIAA Paper 2008-4917
Meeting Information
Meeting: AIAA/ASME/SAE/ASEE Joint Propulsion Conference
Location: Hartford, CT
Country: United States
Start Date: July 20, 2008
End Date: July 23, 2008
Sponsors: American Inst. of Aeronautics and Astronautics, American Society for Electrical Engineers, American Society of Mechanical Engineers, Society of Automotive Engineers, Inc.
Distribution Limits
Public
Copyright
Other
Keywords
electric propulsion

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