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TechEdSat-11 Mission Summary and Survey of Upcoming TES-n MissionsThe TechEdSat (TES) nano-satellite flight series is a collaborative effort from the NASA Ames Research Center engaging young professionals, universities, and other government organizations with next generation space technologies. The 6U TES-11 cube satellite was launched on July 3, 2024, and is currently operating in Low-Earth Orbit. The goal of the mission is to test a variety of next generation communication experiments for nano satellites. The cognitive communication payload, developed by NASA Glenn Research Center, involves the User Initiated Service (UIS) and High Delay Tolerant Networking (HTDN) software packages. First, UIS autonomously schedules radio downlinks and automatically determines an appropriate ground station to use. Next, HDTN then determines how to properly package the data to maximize packets received during a scheduled session. HDTN and UIS both operate on the TES custom S-Band Lunar radio. Alternatively, TES-11 also contains a custom 10-Watt UHF radio from NOAA and developed by Microcom. The goal of the radio experiment is to demonstrate satellite to satellite communications with NOAA GOES and the Eumetsat data collection systems. The TES11 radio experiments have both proven successful in flight. The integration and flight testing of the cognitive communication payload and NOAA payload will be discussed. Additionally, an analysis of iridium short-burst-data (SBD) packet transmission rate during TES-11’s polar orbit are presented; cyclic variance in transmission success rates has been observed, which are attributed to the relative precession rate between Iridium constellation and SSO planes.  The communication experiments will have utility for cis-lunar space applications in optimizing data transfer to earth stations.  Lastly, a preview of upcoming TES missions will  be discussed, including the next flight of the BrainStack (an orbital artificial intelligence and machine learning testbed), an atmospheric Heliophysics test probe architecture,  the Doppler Wind and Temperature Sounder (DWTS) technology demonstrations, and the Exo-Brake (an exo-atmospheric braking device for rapid de-orbit and debris mitigation).
Document ID
20250003838
Acquisition Source
Ames Research Center
Document Type
Presentation
Authors
Marcus S Murbach
(Ames Research Center Mountain View, United States)
Alejandro J Salas
(Millennium Engineering and Integration (United States) Arlington, Virginia, United States)
Malachi Mooney-Rivkin
(Metis Technology Solutions, Inc. Albuquerque, NM)
Avery Brock
(KBR (United States) Houston, Texas, United States)
James P Adams
(University of Idaho Moscow, United States)
Kwabena Boateng
(Millennium Engineering and Integration (United States) Arlington, Virginia, United States)
Jose Alvarellos
(ASRC Federal)
L Seth Schisler
(Ames Research Center Mountain View, United States)
Stanley Krzesniak
(Metis Technology Solutions, Inc. Albuquerque, NM)
Thomas W Hector
(Ames Research Center Mountain View, United States)
Date Acquired
April 16, 2025
Subject Category
Avionics and Aircraft Instrumentation
Spacecraft Instrumentation and Astrionics
Space Radiation
Spacecraft Design, Testing and Performance
Meeting Information
Meeting: CubeSat Developers Workshop
Location: San Luis Obispo, CA
Country: US
Start Date: April 22, 2025
End Date: April 24, 2025
Sponsors: California Polytechnic State University
Funding Number(s)
WBS: 383807.01.21.21.02
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Keywords
TES-n
TechEdSat
TechEdSat-11
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