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Evolution of a Reconfigurable Processing Platform for a Next Generation Space Software Defined RadioThe National Aeronautics and Space Administration (NASA)Harris Ka-Band Software Defined Radio (SDR) is the first, fully reprogrammable space-qualified SDR operating in the Ka-Band frequency range. Providing exceptionally higher data communication rates than previously possible, this SDR offers in-orbit reconfiguration, multi-waveform operation, and fast deployment due to its highly modular hardware and software architecture. Currently in operation on the International Space Station (ISS), this new paradigm of reconfigurable technology is enabling experimenters to investigate navigation and networking in the space environment.The modular SDR and the NASA developed Space Telecommunications Radio System (STRS) architecture standard are the basis for Harris reusable, digital signal processing space platform trademarked as AppSTAR. As a result, two new space radio products are a synthetic aperture radar payload and an Automatic Detection Surveillance Broadcast (ADS-B) receiver. In addition, Harris is currently developing many new products similar to the Ka-Band software defined radio for other applications. For NASAs next generation flight Ka-Band radio development, leveraging these advancements could lead to a more robust and more capable software defined radio.The space environment has special considerations different from terrestrial applications that must be considered for any system operated in space. Each space mission has unique requirements that can make these systems unique. These unique requirements can make products that are expensive and limited in reuse. Space systems put a premium on size, weight and power. A key trade is the amount of reconfigurability in a space system. The more reconfigurable the hardware platform, the easier it is to adapt to the platform to the next mission, and this reduces the amount of non-recurring engineering costs. However, the more reconfigurable platforms often use more spacecraft resources. Software has similar considerations to hardware. Having an architecture standard promotes reuse of software and firmware. Space platforms have limited processor capability, which makes the trade on the amount of amount of flexibility paramount.
Document ID
20140017779
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Kacpura, Thomas J.
(NASA Glenn Research Center Cleveland, OH United States)
Downey, Joseph A.
(NASA Glenn Research Center Cleveland, OH United States)
Anderson, Keffery R.
(Harris Corp. Palm Bay, FL, United States)
Baldwin, Keith
(Harris Corp. Palm Bay, FL, United States)
Date Acquired
December 30, 2014
Publication Date
March 1, 2014
Subject Category
Space Communications, Spacecraft Communications, Command And Tracking
Computer Programming And Software
Report/Patent Number
GRC-E-DAA-TN11787
Meeting Information
Meeting: 2014 IEEE Aerospace Conference
Location: Big Sky, MT
Country: United States
Start Date: March 1, 2014
End Date: March 8, 2014
Sponsors: Institute of Electrical and Electronics Engineers
Funding Number(s)
WBS: WBS 289972.10.03.03
CONTRACT_GRANT: NNC09AA01A
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Telecommunication
International Space Station
Software Defined Radio
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