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Development of a NASA 6-U SatelliteNASA/Wallops Flight Facility has focused on the development of new technologies for the advancement of 6 Unit (6U) small satellites. From the design of the structure and instrument support hardware to improvements in the deployer, NASA is concentrating on maximizing the potential of small satellites for the benefit of science. The telemetry system provides much higher data rates than typical I U UHF system. 6U provides up to several hundred kilobits per second and utilizes the existing NASA Ground Network for data reception. The guidance, navigation and control system keeps the satellite pointed within plus or minus 10 degrees of the sun and has knowledge of the sun vector within 1 degree. The 6U power design increased the options for different voltages and power switching capabilities and is capable of supporting instruments with higher power requirements. The Command & Data Handling (C&DH) system includes a low-power 520 MHz flight processor which provides more processing capability than existing I U processor technologies. These optimized technologies will offer the science community a greater opportunity for flying more sophisticated and complex instruments.
Document ID
20110015185
Acquisition Source
Goddard Space Flight Center
Document Type
Abstract
Authors
Thompson, Linda D.
(NASA Wallops Flight Center Wallops Island, VA, United States)
Date Acquired
August 25, 2013
Publication Date
August 8, 2011
Subject Category
Spacecraft Instrumentation And Astrionics
Report/Patent Number
GSFC.ABS.4908.2011
Report Number: GSFC.ABS.4908.2011
Meeting Information
Meeting: AIAA/USU Conference on Small Satellites
Location: Logan, UT
Country: United States
Start Date: August 8, 2011
End Date: August 11, 2011
Sponsors: American Inst. of Aeronautics and Astronautics, Utah State Univ.
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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