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ROCKET-SPACE COMPLEX AND METHOD OF FUNCTIONING OF THE ROCKET-SPACE COMPLEX

机译:火箭-空间复合物及其功能方法

摘要

FIELD: aviation.SUBSTANCE: group of inventions relates to means and methods of launch, orbit and de-orbit automatic payloads (PL) using unmanned rocket and space complex (RSC). The RSC includes an upper stage (US) with control devices for the launch vehicle, which, when separating PL from the US, remotely control the service systems of PL, the fuel reserve for PL disengagement, the docking system with PL in the working orbit and the manipulator for maintenance and installation of PL on US. PL can be performed and inseparable from US. LF or remote control of the PL, after its separation, the US is moved to the specified place of the orbit. The power supply of PL is carried out with the use of equipment delivered by US or from standard airborne systems of US. The PL deorbit is carried out with the help of US, after its rapprochement and docking with it.EFFECT: minimization of control and power systems of the rocket and space complex, simplification of the process of launching into orbit, the possibility of complete subsequent utilisation of the components of rocket and space complex.2 cl, 4 dwg
机译:技术领域:一组发明涉及使用无人火箭和航天综合体(RSC)进行发射,轨道和脱离轨道的自动有效载荷(PL)的装置和方法。 RSC包括一个带有运载火箭控制装置的上级装置(US),当将PL与美国分开时,该装置可远程控制PL的服务系统,PL脱离的燃油储备,PL在工作轨道上的对接系统以及用于在美国维护和安装PL的机械手。 PL可以执行,与美国密不可分。 LF或PL的遥控器,在分离之后,将美国移动到指定的轨道位置。 PL的电源使用美国提供的设备或美国标准机载系统提供。 PL轨道在和解与对接后由美国协助进行。效果:最小化火箭和太空综合体的控制和动力系统,简化了送入轨道的过程,有可能完全被随后利用火箭和太空综合体的组成部分。2cl,4 dwg

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