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2-BLADES DEPLOYING BY CENTRIFUGAL FORCE SOLAR SAIL EXPERIMENT

机译:离心力太阳帆实验在2叶片展开中的应用

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Up to the present moment there have been not many pico-and nanosatellite missions with high energy interorbitalor interplanetary transfers. Ones of the reasons are the adaptation difficulties of the traditional propulsion devices,such as liquid or solid propellant engines. Solar sail as a propulsion device was proposed to solve this problem.But, we get lots of problems while realising this type of propulsion. These problems are solar sail deployment,solar sail control and limitation for the solar sail area in spacecraft mass ratio. We have designed the solutions ofthese problems. According on these solutions we have designed the construction of 2-bladed solar sail deploying bycentrifugal force. The feature of the proposed sail is the impossibility of performing development tests in groundconditions. That's why we have to perform these tests just in Space.The Project of solar sail developing called BMSTU-Sail. We proposed the experiment roadmap, which consistsof two milestones:1. The LEO experiment without large solar sail deployment. Overall solar sail area is 0.15 m~2 and area-mass ratiois 0.3 square meters per kilogram. In this mission we are going to test the solar sail deploying subsystem. Forthis purpose, we developed the experimental pico-satellite for the launching from the ISS.2. The MEO experiment with large solar sail deployment. We are going to deploy 30 m~2 solar sail, using theresults obtained on the previous stage. During the flight we are going to verify solar sail mathematical modelfor future implementation and try to make the interorbital transfer.The paper presents the solution of the solar sail dynamics problems, associated with its deployment. This papertells us about the pico-satellite designed for realization of the 1st experiment milestone. Also this paper includes theinformation about the launching device from the ISS and the ground segment devices. In addition to the solar saildeployment experiment we are going to prove the possibility of this construction to be used for space debris deorbit.The other goal of this experiment is to provide the amateur radio communication to make the space sciencepromotion for students.This work is conducting by the group of about 30 students based on the BMSTU Youth Space Centre. Accordingon the results of this work we are going to unite all the BMSTU research and develop capabilities in a very greatchallenge - the developing student-made interplanetary mission to the Moon.
机译:到目前为止,还没有多少具有高能轨道间的微微和纳米卫星飞行任务 或行星际转移。原因之一是传统推进装置的适应困难, 例如液体或固体推进剂发动机。为了解决这个问题,提出了将太阳帆作为推进装置。 但是,在实现这种推进方式时,我们会遇到很多问题。这些问题是太阳帆的部署, 太阳帆的控制和对航天器质量比中太阳帆区域的限制。我们设计了以下解决方案 这些问题。根据这些解决方案,我们设计了2叶片太阳帆的构造 离心力。拟议中的帆的特点是不可能在地面上进行开发测试 情况。这就是为什么我们必须仅在太空中执行这些测试的原因。 太阳帆开发项目称为BMSTU-Sail。我们提出了实验路线图,其中包括 两个里程碑: 1.没有大型太阳帆部署的LEO实验。太阳帆总面积为0.15 m〜2且面积质量比 是每公斤0.3平方米。在此任务中,我们将测试太阳帆部署子系统。为了 为此,我们开发了用于从国际空间站发射的实验性微卫星。 2.大型太阳帆部署的MEO实验。我们将使用30m〜2的太阳帆 在上一阶段获得的结果。在飞行过程中,我们将验证太阳帆的数学模型 为了将来的实现,并尝试进行轨道间转移。 本文介绍了太阳帆动力学问题及其解决方案的解决方案。这篇报告 向我们介绍了为实现第一个实验里程碑而设计的微微卫星。此外,本文还包括 有关来自国际空间站和地面部分设备的发射设备的信息。除了太阳帆 部署实验中,我们将证明这种构造可用于空间碎片轨道的可能性。 该实验的另一个目标是提供业余无线电通信以制作太空科学 促进学生。 这项工作由BMSTU青年空间中心的大约30名学生组成。根据 根据这项工作的结果,我们将团结所有BMSTU的研究和开发能力, 挑战-不断发展的学生制作的月球行星际飞行任务。

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