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Measurement of the directional distribution of incident particles in the Shuttle-Mir mission orbit

机译:航天飞机-米尔飞行任务轨道上入射粒子定向分布的测量

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The measurement of the directional distribution of incident particles was made by using the Real time Radiation Monitoring Device (RRMD)-III placed inside the Space Shuttle STS-84 cruised at an altitude of 400 km and an inclination angle of 51.6 deg, which are the same as the cruising orbit of the International Space Station (ISS). The directional distributions of incident particles were evaluated over the observed linear energy transfer (LET) range (1-100 keV/#mu#m). The pitch angle distribution is also obtained using the geomagnetic model of IGRF-95. The result is roughly in good agreement with the distribution obtained by the VF1-MIN anisotropy model calculation within the present experimental errors, if the shielding distribution is assumed to be uniform.
机译:通过使用放置在STS-84航天飞机内的实时辐射监测装置(RRMD)-III来测量入射粒子的方向分布,该航天飞机以400公里的高度和51.6度的倾角巡航,与国际空间站(ISS)的巡航轨道相同。在观察到的线性能量转移(LET)范围(1-100 keV /#mu#m)上评估了入射粒子的方向分布。使用IGRF-95的地磁模型也可以获得俯仰角分布。如果假设屏蔽分布均匀,则结果与在当前实验误差范围内通过VF1-MIN各向异性模型计算获得的分布大致吻合。

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