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Solidifying Small Satellite Access to Orbit via the International Space Station (ISS): Cyclops' Deployment of the Lonestar SmallSat from the ISSOn January 29, 2016, the Space Station Integrated Kinetic Launcher for Orbital Payload Systems (SSIKLOPS), known as "Cyclops" to the International Space Station (ISS) community, deployed Lonestar from the ISS. The deployment of Lonestar, a collaboration between Texas A&M University and the University of Texas at Austin, continued to showcase the simplicity and reliability of the Cyclops deployment system. Cyclops, a NASA-developed, dedicated 10-100 kg class ISS SmallSat deployment system, utilizes the Japanese airlock and robotic systems to seamlessly insert SmallSats into orbit. This paper will illustrate Cyclops' successful deployment of Lonestar from the ISS as well as outline its concept of operations, interfaces, requirements, and processes.
Document ID
20160007871
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Hershey, Matthew P.
(NASA Johnson Space Center Houston, TX, United States)
Newswander, Daniel R.
(NASA Johnson Space Center Houston, TX, United States)
Evernden, Brent A.
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
June 23, 2016
Publication Date
August 6, 2016
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
SSC16-II-04
JSC-CN-36516
Meeting Information
Meeting: AIAA Small Satellite Conference
Location: Logan, UT
Country: United States
Start Date: August 6, 2016
End Date: August 11, 2016
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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