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Near Earth Asteroid Solar Sail Engineering Development Unit Test ProgramThe Near Earth Asteroid (NEA) Scout project is a 30x20x10cm (6U) cubesat reconnaissance mission to investigate a near Earth asteroid utilizing an 86m2 solar sail as the primary propulsion system. This will be the largest solar sail NASA will launch to date. NEA Scout is a secondary payload currently manifested on the maiden voyage of the Space Launch System in 2018. In development of the solar sail subsystem, design challenges were identified and investigated for packaging within a 6U form factor and deployment in cis-lunar space. Analysis furthered understanding of thermal, stress, and dynamics of the stowed system and matured an integrated sail membrane model for deployed flight dynamics. This paper will address design, fabrication, and lessons learned from the NEA Scout solar sail subsystem engineering development unit. From optical properties of the sail material to folding and spooling the single 86m2 sail, the team has developed a robust deployment system for the solar sail. This paper will also address expected and received test results from ascent vent, random vibration, and deployment tests.
Document ID
20170001496
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Lockett, Tiffany Russell
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Few, Alexander
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Wilson, Richard
(Jacobs Engineering and Science Services and Skills Augmentation Group (ESSSA) Huntsville, AL, United States)
Date Acquired
February 9, 2017
Publication Date
January 17, 2017
Subject Category
Engineering (General)
Report/Patent Number
M17-5763
Meeting Information
Meeting: International Symposium on Solar Sailing (ISSS 2017)
Location: Kyoto
Country: Japan
Start Date: January 17, 2017
End Date: January 20, 2017
Distribution Limits
Public
Copyright
Public Use Permitted.
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