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  • PhoneSat: a smartphone-based spacecraft bus

    Paper number

    IAC-11,B4,6B,9,x10655

    Author

    Dr. William Marshall, National Aeronautics and Space Administration (NASA)/Marshall Space Flight Center, United States

    Coauthor

    Dr. Christopher Boshuizen, National Aeronautics and Space Administration (NASA)/Ames Research Center, United States

    Coauthor

    Mr. Benjamin Howard, United States

    Coauthor

    Mr. Michael Safyan, International Space University (ISU), France

    Coauthor

    Mr. Matthew Leines, Air Force Research Laboratory (AFRL), United States

    Coauthor

    Mr. James Snow, National Aeronautics and Space Administration (NASA), United States

    Coauthor

    Mr. Vincent Beukelaers, National Aeronautics and Space Administration (NASA), United States

    Coauthor

    Ms. Carmen Felix, Space Safety Magazine, Mexico

    Year

    2011

    Abstract
    Motivated to find transformation reductions in cost and development time of spacecraft, we examine the use of smartphones as the basis of a satellite bus. Today’s smartphones have most of the core capabilities of a spacecraft: a fast processor and large memory capacity; a range of sensors such as accelerometers, rate gyros, magnetometers and GPS; batteries and power management; several radios; and high resolution cameras. Companies investing in smartphones have spent billions of dollars to squeeze sophisticated capability into a small, physically robust form-factor, and they now mass-produce devices in enormous volumes, lowering costs substantially.
    
    Beginning in mid-2009 as a student-let effort, the PhoneSat project at NASA Ames set out to test the hypothesis of whether such COTS hardware can be used as the basis of workable ultra cheap satellite busses. In this paper we outline an approach whereby smartphones can be used as a wholesale replacement for the core computer systems, as well as most of the core sensor capabilities, of a spacecraft. We detail the bus design and ground-based environmental testing that has been performed; we provide the results from integrated field tests on balloons and sub-orbital rockets; finally we share lessons learnt on the engineering approaches taken, including the projects adoption of rapid prototyping techniques. We show that it is possible to design and build from scratch a spacecraft within 2 weeks and for under \$10,000.  Spacecraft based on this low-cost approach could enable a myriad of new spacecraft missions, and a whole new class of missions involving large constellations could become viable.
    Abstract document

    IAC-11,B4,6B,9,x10655.brief.pdf

    Manuscript document

    IAC-11,B4,6B,9,x10655.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.