• DocumentCode
    2905517
  • Title

    Science of opportunity: Heliophysics on the FASTSAT mission and STP-S26

  • Author

    Rowland, Douglas E. ; Collier, Michael R. ; Sigwarth, John B. ; Jones, Sarah L. ; Hill, Joanne K. ; Benson, Robert ; Choi, Michael ; Chornay, Dennis ; Cooper, John ; Feng, Steven ; Gill, Nathaniel ; Goodloe, Colby ; Han, Lawrence ; Hancock, Holly ; Hunsak

  • Author_Institution
    NASA Goddard Space Flight Center, Greenbelt, MD, USA
  • fYear
    2011
  • fDate
    5-12 March 2011
  • Firstpage
    1
  • Lastpage
    12
  • Abstract
    The FASTSAT spacecraft, which was launched on November 19, 2010 on the DoD STP-S26 mission, carries three instruments developed in joint collaboration by NASA GSFC and the US Naval Academy: PISA, TTI, and MINI-ME.1,2 As part of a rapid-development, low-cost instrument design and fabrication program, these instruments were a perfect match for FASTSAT, which was designed and built in less than one year. These instruments, while independently developed, provide a collaborative view of important processes in the upper atmosphere relating to solar and energetic particle input, atmospheric response, and ion outflow. PISA measures in-situ irregularities in electron number density, TTI provides limb measurements of the atomic oxygen temperature profile with altitude, and MINI-ME provides a unique look at ion populations by a remote sensing technique involving neutral atom imaging. Together with other instruments and payloads on STP-S26 such as the NSF RAX mission, FalconSat-5, and NanoSail-D (launched as a tertiary payload from FASTSAT), these instruments provide a valuable “constellation of opportunity” for following the flow of energy and charged and neutral particles through the upper atmosphere. Together, and for a small fraction of the price of a major mission, these spacecraft will measure the energetic electrons impacting the upper atmosphere, the ions leaving it, and the large-scale plasma and neutral response to these energy inputs. The result will be a new model for maximizing scientific return from multiple small, distributed payloads as secondary payloads on a larger launch vehicle.
  • Keywords
    aerospace instrumentation; atmospheric measuring apparatus; remote sensing; space vehicles; AD 2010 11 19; DoD STP-S26 mission; FASTSAT mission; FASTSAT spacecraft; FalconSat-5; MINI-ME; NASA GSFC; NSF RAX mission; NanoSail-D; PISA; TTI; US Naval Academy; atomic oxygen temperature profile; electron number density; energetic electrons; fabrication program; heliophysics; ion outflow; ion populations; limb measurements; low-cost instrument design; neutral atom imaging; remote sensing technique; upper atmosphere; Aerospace electronics; Atmospheric measurements; Instruments; Payloads; Space vehicles; Temperature measurement;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2011 IEEE
  • Conference_Location
    Big Sky, MT
  • ISSN
    1095-323X
  • Print_ISBN
    978-1-4244-7350-2
  • Type

    conf

  • DOI
    10.1109/AERO.2011.5747235
  • Filename
    5747235