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Design, Development and Testing of the GMI Launch LocksBall Aerospace will deliver the GPM Microwave Imager (GMI), to NASA as one of the 3 instruments to fly on the Global Precipitation Measurement (GPM) mission, for launch in 2013. The radiometer, when deployed, is over 8 feet tall and rotates at 32 revolutions per minute (RPM) can be described as a collection of mechanisms working to achieve its scientific objectives. This collection precisely positions a 1.2 meter reflector to a 48.5 degree off nadir angle while rotating, transferring electrical power and signals to and from the RF receivers, designs two very stable calibration sources, and provides the structural integrity of all the components. There are a total of 7 launch restraints coupling across the moving and stationary elements of the structure,. Getting from design to integration will be the focus of this paper.
Document ID
20110016488
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Sexton, Adam
(Ball Aerospace and Technologies Corp. Boulder, CO, United States)
Dayton, Chris
(Ball Aerospace and Technologies Corp. Boulder, CO, United States)
Wendland, Ron
(Ball Aerospace and Technologies Corp. Boulder, CO, United States)
Pellicciotti, Joseph
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
August 25, 2013
Publication Date
September 28, 2011
Subject Category
Spacecraft Instrumentation And Astrionics
Report/Patent Number
NF1676L-12197
Report Number: NF1676L-12197
Meeting Information
Meeting: 14th European Space Mechanism and Tribology Symposium
Location: Constance
Country: Germany
Start Date: September 28, 2011
End Date: September 30, 2011
Sponsors: European Space Agency, Centre National d'Etudes Spatiales
Funding Number(s)
WBS: WBS 869021.03.07.01.06
Distribution Limits
Public
Copyright
Public Use Permitted.
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