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
Link To Document :
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