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机构地区:[1]北京控制工程研究所推进中心,北京100080
出 处:《宇航学报》2007年第2期503-507,共5页Journal of Astronautics
摘 要:为了对国外新型卫星推进剂贮箱的研究动态进行跟踪,对第二代表面张力贮箱的研究与应用进展做了阐述。首先对比了不同类型推进剂贮箱的特点,在此基础上,从试验研究、数值模拟和实际应用三个角度对第二代表面张力贮箱——以板式结构为主的表面张力贮箱的发展做了综述。研究表明,国际上已经对第二代表面张力贮箱的性能做了大量的数值模拟和搭载试验,如今第二代表面张力贮箱已经成为当今国际大型卫星推进剂贮箱的主流。这为新型卫星推进剂贮箱的研究指明方向并提供有价值的参考。In order to track the developmental trends of satellite propellant tank, the evolvement of the second generation surface tension tank, in which the vane type Propellant management device was uesd, was reviewed in the paper. The characters of different propellant tanks were compared firstly. Then the developments of the vane type surface tension tank, such as flight experiments on the space, numerical simulations for its flow performance and application on satellites, were reviewed in detail. The results show that the study on the vane type surface tension tank is full enough, and this kind of tank has been applied in several main satellite platforms successfully. The paper can provide references for studying and designing the second generation surface tension tank.
关 键 词:表面张力贮箱 推进剂管理装置 板式 搭载试验 数值模拟
分 类 号:V421.33[航空宇航科学与技术—飞行器设计]
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