Russian Institute for Space Device Engineering Science Research Institute for Precision Device Engineering
➤ Gửi thông báo lỗi ⚠️ Báo cáo tài liệu vi phạmNội dung chi tiết: Russian Institute for Space Device Engineering Science Research Institute for Precision Device Engineering
Russian Institute for Space Device Engineering Science Research Institute for Precision Device Engineering
Russian Institute for Space Device EngineeringScience Research Institute for Precision Device EngineeringAPPROVEDChief Designer of the orderV. Shargor Russian Institute for Space Device Engineering Science Research Institute for Precision Device Engineeringrodsky","1997WESTPAC Satellite.The Scientific-Technical note for userMoscow 19972CONTENTS1Purpose of WESTPAC satellite.32General information about WESTPAC satellite.33The main design parameters of detachable satellite WESTPAC and temperatureinfluence evaluation results on it’s design in the conditio Russian Institute for Space Device Engineering Science Research Institute for Precision Device Engineeringns of orbital flight._64Description of satellite optical-mechanical mathematical model. Calculation of energy and accuracy parameters of WESTPAC satelRussian Institute for Space Device Engineering Science Research Institute for Precision Device Engineering
lite.234.1.Optical configuration of WESTPC satellite.____________________________________234.2.Grounds for selection of type of prism RRs for WESTPAC Russian Institute for Space Device EngineeringScience Research Institute for Precision Device EngineeringAPPROVEDChief Designer of the orderV. Shargor Russian Institute for Space Device Engineering Science Research Institute for Precision Device Engineeringf accuracy and energy parameters of WESTPAC satellite.264.5.Analysis of results of energy and accuracy calculations.345Control of reflection pattern of WESTPAC satellite.355.1. Basic technical characteristics of measurement system during theregistration of reflection pattern.375.2 Short description Russian Institute for Space Device Engineering Science Research Institute for Precision Device Engineeringof the design and functioning control-measuring bench._______376Mechanical tests of WESTPAC satellite.397The checkout and minimization of WESTPAC sateRussian Institute for Space Device Engineering Science Research Institute for Precision Device Engineering
llitefabrication andassembling RMSE.________________________________418WESTPAC satellite main parameters 459Conclusion.513The Scientific-technical notRussian Institute for Space Device EngineeringScience Research Institute for Precision Device EngineeringAPPROVEDChief Designer of the orderV. Shargor Russian Institute for Space Device Engineering Science Research Institute for Precision Device Engineeringnd laser stations for laser ranging. Energy and accuracy satellite parameters given in the present note are defined with the use of adjusted mathematics model, and the satellite design IS described taking into account adjustments based on production results, experimental bench testing and final adju Russian Institute for Space Device Engineering Science Research Institute for Precision Device Engineeringstment of satellite optical-mechanical design at the final stage of development.1Purpose of WESTPAC satelliteWESTPAC satellite is designed for reflectRussian Institute for Space Device Engineering Science Research Institute for Precision Device Engineering
ion of incoming ground laser rangers’ radiation with the purpose to measure distance to the satellite's center of mass. In addition, the satellite is Russian Institute for Space Device EngineeringScience Research Institute for Precision Device EngineeringAPPROVEDChief Designer of the orderV. Shargor Russian Institute for Space Device Engineering Science Research Institute for Precision Device Engineeringosition WESTPAC satellite must be in condition of free non-oriented flight on altitude of about 835 km above the Earth surface.2General information about WESTPAC satelliteWESTPAC satellite is a system of 60 prism corner cube retroreflectors (RR) fixed in holders in the monolith spherical body. The m Russian Institute for Space Device Engineering Science Research Institute for Precision Device Engineeringain feature of the satellite is minimum error of link of range measurements to its center of mass - 0.5 mm. This IS achieved by such satellite's desigRussian Institute for Space Device Engineering Science Research Institute for Precision Device Engineering
n that laser light of SLR station incoming from any direction, is reflected only by one reflector with the field of view limited by the lens shading. Russian Institute for Space Device EngineeringScience Research Institute for Precision Device EngineeringAPPROVEDChief Designer of the orderV. ShargorRussian Institute for Space Device EngineeringScience Research Institute for Precision Device EngineeringAPPROVEDChief Designer of the orderV. ShargorGọi ngay
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