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The TechEdSat-N Series: A Collaborative Technology Development Platform in the Nano-Satellite Form FactorThe TechEdSat-1 (TES-1) was the first U.S. CubeSat to be deployed from the ISS (International Space Station). This permitted the initiation of a flight series that has recently de-orbited the 6th nano-satellite with subsequent numbers 7-10 under development. The nano-satellites range from 1U (1 unit) to 6U (TechEdSat-8) but have the critical ISS Safety design features standardized in order to focus on the particular experiment objectives. Incremental experimental development has included unique communication subsystems such as command/control of the nanosatellite through email commands -as well as a recent record for Wifi transmission. Also, the thermophysics of controlled drag devices (Exo-Brake) has been developed which will prelude sample return and planetary exploration applications. The successful "rapid incremental experiment" approach has also been incorporated into collaborations with academia, permitting professors/student interns to be exposed to the rigors of space mission hardware design and execution. The TechEdSat-8, a linear 6U configuration, allows for 5 different groups to contribute an "experiment, sensor, or sub-system" through a well-defined common interface. Lastly, the flying laboratory concept is helpful in developing future interplanetary nano-satellite subsystems which will advance exploration goals by allowing rapid demonstration/validation first in LEO (Low Earth Orbit).
Document ID
20190002596
Acquisition Source
Ames Research Center
Document Type
Abstract
Authors
Murbach, M. S,
(NASA Ames Research Center Moffett Field, CA, United States)
Guarneros, A.
(NASA Ames Research Center Moffett Field, CA, United States)
Alena, R.
(NASA Ames Research Center Moffett Field, CA, United States)
Papadopoulos, P.
(San Jose State Univ. San Jose, CA, United States)
Tanner, F.
(Millennium Engineering and Integration Co. Moffett Field, CA, United States)
Wheless, J.
(Millennium Engineering and Integration Co. Moffett Field, CA, United States)
Smith, S.
(American Paragon Protective Services Leander, TX, United States)
Salas, A.
(Millennium Engineering and Integration Co. Moffett Field, CA, United States)
Williams, N.
(San Jose State Univ. San Jose, CA, United States)
Date Acquired
April 18, 2019
Publication Date
July 23, 2018
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
ARC-E-DAA-TN56618
Meeting Information
Meeting: International Space Station Research & Development Conference (ISSR&D 2018)
Location: San Francisco , CA
Country: United States
Start Date: July 23, 2018
End Date: July 26, 2018
Sponsors: NASA Headquarters, Center for the Advancement of Science in Space (CASIS), American Astronautical Society
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Small Payload Quick Return
SmallSatellites
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