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1.
Adv Space Res ; 12(2-3): 331-4, 1992.
Article in English | MEDLINE | ID: mdl-11537025

ABSTRACT

An X2/2B level solar flare occurred on 12 August, 1989, during the last day of the flight of the Space Shuttle Columbia (STS-28). Detectors on the GOES 7 satellite observed increased X-ray fluxes at approximately 1400 GMT and a solar particle event (SPE) at approximately 1600 GMT. Measurements with the bismuth germanate (BGO) detector of the Shuttle Activation Monitor (SAM) experiment on STS-28 showed factors of two to three increases in count rates at high latitudes comparable to those seen during South Atlantic Anomaly (SAA) passages beginning at about 1100 GMT. That increased activity was observed at both north and south high latitudes in the 57 degrees, 300 kilometer orbit and continued until the detector was turned off at 1800 GMT. Measurements made earlier in the flight over the same geographic coordinates did not produce the same levels of activity. This increase in activity may not be entirely accounted for by observed geomagnetic phenomena which were not related to the solar flare.


Subject(s)
Gamma Rays , Radiation Monitoring/instrumentation , Solar System , Space Flight/instrumentation , Spacecraft/instrumentation , Bismuth , Germanium , Magnetics , Protons , Radiation Protection , Radiometry , Sodium Iodide
2.
Adv Space Res ; 12(2-3): 461-4, 1992.
Article in English | MEDLINE | ID: mdl-11537045

ABSTRACT

The Shuttle Activation Monitor (SAM) experiment was flown on the Space Shuttle Columbia (STS-28) from 8-13 August, 1989 in a 57 degrees, 300 km orbit. One objective of the SAM experiment was to determine the relative effect of different amounts of shielding on the gamma-ray backgrounds measured with similarly configured sodium iodide (NaI) and bismuth germante (BGO) detectors. To achieve this objective twenty-four hours of data were taken with each detector in the middeck of the Shuttle on the ceiling of the airlock (a high-shielding location) as well as on the sleep station wall (a low-shielding location). For the cosmic-ray induced background the results indicate an increased overall count rate in the 0.2 to 10 MeV energy range at the more highly shielded location, while in regions of trapped radiation the low shielding configuration gives higher rates at the low energy end of the spectrum.


Subject(s)
Cosmic Radiation , Gamma Rays , Radiation Monitoring/standards , Radiation Protection/standards , Space Flight , Spacecraft/standards , Aluminum/standards , Bismuth , Gold/standards , Nickel/standards , Protons , Radiation Monitoring/instrumentation , Radiation Monitoring/methods , Radiation Protection/instrumentation , Radiation Protection/methods , Sodium Iodide , Spacecraft/instrumentation , Thermoluminescent Dosimetry
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