@techreport{oai:jaxa.repo.nii.ac.jp:00006013,
 author = {松本, 晴久 and 越石, 英樹 and 五家, 建夫 and Matsumoto, Haruhisa and Koshiishi, Hideki and Goka, Tateo},
 month = {Nov},
 note = {The onboard electronic devices and astronauts on spacecrafts have many effects on the space radiation. It is one of the important issues for space mission planning to predict the space radiation environment and to evaluate it. Because the space vehicles must be designed to decrease the radiation exposure to protect devices and astronauts. Among many kinds of radiation in space, the radiation belts particles having continuously high fluxes give a large dose contribution to a near-earth space mission. The radiation belts have been measured with various satellites and detectors. NASA's radiation belt models, AP8 (Sawyer and Vette, 1976) and AE8 (Vette, 1991) were derived from the data which had been observed in the 1960s and 1970s. In the recent, CRRES models have been developed with the data of the CRRES satellite (Gussenhoven et al., 1996). NOAAPRO (NOAA proton) model have been developed with the data of the NOAA-TIROS satellite (Huston, 1998). POLE model have been developed with the data of the LANL's geostationary satellite (Boscher et al., 2003). We have developed the radiation belt models (beta version) using MDS-1 data., 資料番号: AA0049500029, レポート番号: JAXA-SP-06-006},
 title = {宇宙放射線帯モデルの開発},
 year = {2006}
}