摘要
建立了一个较为理想情况下卫星表面原子氧通量和遭遇量的计算模式．在此基础上，着重讨论了轨道高度、太阳活动、飞行攻角及轨道倾角等因素对原子氧通量和遭遇量的影响．
In this paper, a model for computing Atomic Oxygen (AO) flux and fluenceis developed under relatively ideal conditions. The effects of some factors (orbitaltitude, solar activity, incident angle and inclination) on AO flux and fluence aremainly discussed.
出处
《空间科学学报》
CAS
CSCD
北大核心
1999年第2期167-172,共6页
Chinese Journal of Space Science
