• DocumentCode
    2065342
  • Title

    Multi-band software defined radio for spaceborne communications, navigation, radio science, and sensors

  • Author

    Haskins, Christopher B. ; Millard, Wesley P.

  • Author_Institution
    Appl. Phys. Lab., Johns Hopkins Univ., Laurel, MD, USA
  • fYear
    2010
  • fDate
    6-13 March 2010
  • Firstpage
    1
  • Lastpage
    9
  • Abstract
    Demanding mass and power requirements across many low-cost NASA mission sets (Discovery, New Frontiers, Mars Scout, SMEX, MIDEX, and others) place a premium on lightweight, efficient, and versatile radios. A low power, low mass, modular, multi-band software-defined radio (SDR) has been developed by JHU/APL, under the name Frontier Radio, for use in communications, navigation, radio science, and sensor applications for a variety of NASA missions. The current SDR implementation features communications and Doppler navigation modes, and provides a highly capable platform to build upon for future technology enhancements. Features such as in-band channel assignment, bit rate, modulation format, turnaround ratio, loop bandwidths, and coding formats are reconfigurable in flight. Modularity within the core hardware and firmware platforms enable infusion of new technology with minimal non-recurring engineering (NRE) costs. Current configurations operate within the NASA S, X (under development), and Ka-bands (26 and 32 GHz), though alternate RF slices may be added and/or substituted for other bands or sensor applications. This SDR is currently capable of transmit data rates up to 25 Mbps (and higher with 8/16 PSK/QAM) and receive data rates up to 1.3 Mbps via QPSK, with significantly higher capability under development. Compatibility with NASA´s STRS architecture helps promote the use of this SDR throughout the NASA community. Along with its low power (5 W receive mode w/internal ovenized oscillator and 28 V bus power) and low mass (1.8/2.1 kg, single/dual band configuration), this SDR offers missions a combination of capabilities and efficiency. The NASA Radiation Belt Storm Probes (RBSP) mission is currently developing a flight implementation of this SDR (S-Band only), with launch planned for the year 2012.
  • Keywords
    modulation coding; software radio; space communication links; Doppler navigation modes; Frontier radio; Ka-bands; NASA mission sets; bit rate; coding formats; firmware platforms; frequency 26 GHz; frequency 32 GHz; in-band channel assignment; loop bandwidths; modulation format; multiband software defined radio; nonrecurring engineering costs; power 5 W; radiation belt storm probes mission; radio science; sensors; spaceborne communications; spaceborne navigation; turnaround ratio; voltage 28 V; Application software; Bandwidth; Bit rate; Hardware; Mars; Modulation; NASA; Radio navigation; Software radio; Space technology;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2010 IEEE
  • Conference_Location
    Big Sky, MT
  • ISSN
    1095-323X
  • Print_ISBN
    978-1-4244-3887-7
  • Electronic_ISBN
    1095-323X
  • Type

    conf

  • DOI
    10.1109/AERO.2010.5446908
  • Filename
    5446908