The invention discloses a thruster support for installation of a small satellite, and relates to the technical field of satellites and application. The thruster support for installation of the small satellite comprises an installation ring, fixed supporting legs are fixedly installed at the bottom of the installation ring, fixed fins are fixedly installed at the lower ends of the sides, away from the center of the bottom of the installation ring, of the fixed supporting legs, a buffering mechanism is arranged at the bottoms of the fixed supporting legs, and a transmission mechanism is arranged on the inner side of the buffering mechanism. The buffering mechanism comprises a fixed plate, a movable groove, a rotating block, a contact piece and a resistance piece, and the fixed plate is fixedly installed at the bottom of the fixed supporting legs. According to the thruster support for installation of the small satellite, the buffering mechanism and the transmission mechanism are arranged, the thruster support is prevented from shaking in the installation and transportation process, and when the small satellite is launched, the situation that the lower ends of the fixing supporting legs make contact with the front face of air, resistance is formed, and fuel consumption is increased when the thruster works is avoided.
本发明公开了一种小型卫星安装用推力器支架,涉及卫星及应用技术领域。该小型卫星安装用推力器支架,包括安装环,所述安装环的底部固定安装有固定支脚,所述固定支脚远离安装环底部中心的一侧下端固定安装有固定鳍片,所述固定支脚的底部设置有缓冲机构,所述缓冲机构的内侧设置有传动机构,所述缓冲机构包括固定板、活动槽、转动块、接触件和阻力件,所述固定板固定安装在固定支脚的底部。该小型卫星安装用推力器支架,设置缓冲机构和传动机构,避免了推力器支架在安装运输过程中发生晃动,且在小卫星发射时避免了固定支脚下端与空气正面接触,形成阻力,加大推力器工作时的燃料消耗。
Thruster support for small satellite installation
一种小型卫星安装用推力器支架
2022-01-21
Patent
Electronic Resource
Chinese
IPC: | B64G Raumfahrt , COSMONAUTICS |
New Electrostatic Thruster for Small Satellite Application
British Library Conference Proceedings | 2000
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