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Science of Opportunity: Heliophysics on the FASTSAT Mission and STP-S26

Authors :
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
Hunsaker, Floyd
Jones, Noble
Keller, John W
Klenzing, Jeffrey
Kleyner, Igor
Moore, Tom
Ogilvie, Keith
Boudreaux, Mark
Casas, Joseph
Myre, David
Smith, Billy
Publication Year :
2011
Publisher :
United States: NASA Center for Aerospace Information (CASI), 2011.

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, TTl, and MINI_ME.I,1 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, TIl provides limb measurements of the atomic oxygen temperature profile with altitude, and MINI-ME provides a unique look at ion populations by a remote sen sing 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 now 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.

Details

Language :
English
Database :
NASA Technical Reports
Publication Type :
Report
Accession number :
edsnas.20120012568
Document Type :
Report
Full Text :
https://doi.org/10.1109/AERO.2011.5747235