以乌斯提诺夫命名的BSTU«VOENMEH»在小型航天器方面的研究和发展的主要方向和一些成果

M. Kislitsky
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摘要

小型航天器的发展需要解决一些新的科学技术问题。以乌斯提诺夫命名的波罗的海国立技术大学VOENMEH的主要研究和发展方向是解决制造小型航天器,部署和维护小型航天器的轨道星座以及管理轨道分组的问题。介绍了这些工作的一些结果,特别是小型空间拖船的初步设计,该拖船采用创新的由氧气和氢气驱动的双组分燃气火箭发动机,与超轻型运载火箭一起运行。小型空间拖船解决了小型航天器的轨道间运输问题。它在俄罗斯的火箭和太空技术中没有类似的东西。为了提高空间通信系统和地球遥感的效率,提出了小航天器弹道耦合群的变型,以保证在轨道上形成稳定的准静止分布孔径。介绍了一种基于压电驱动的新型驱动机构——两轴旋转平台的研制。该装置在重量、尺寸、动态特性等参数方面明显优于传统的基于电驱动的机电设备。考虑了该旋转平台在小型航天器服务系统和目标系统中的应用变化。它显示了这如何能够大大增加小型航天器的战术和技术特性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
The main directions of research and development of BSTU «VOENMEH» named after D. F. Ustinov on the subject of small spacecraft and some results
The development of small spacecrafts requires the solution of a number of new scientific and technical problems. The main directions of research and development of the Baltic State Technical University «VOENMEH» named after D. F .Ustinov on solving the problems of creating small spacecrafts, deploying and maintaining orbital constellations of the small spacecrafts, and managing orbital groupings are presented. Some results of these works are presented, in particular, the preliminary design of a small space tug with an innovative two-component gas rocket engine powered by oxygen and hydrogen, operated in conjunction with an ultralight class launch vehicle. Small space tug solves the problems of interorbital transportation of the small spacecrafts. It has no analogues in the russian rocket and space technology. Variants of ballistically coupled groups of small spacecrafts are presented that can ensure the formation of a stable quasi-stationary distributed aperture in orbits in order to increase the efficiency of space communication systems and remote sensing of the Earth. The development of an innovative actuator – a two-axis rotary platform based on piezoelectric drives is presented. This device significantly exceeds traditional electromechanical devices based on electric drives in terms of weight, dimensions, dynamic characteristics and other parameters. The variants of the application of this rotary platform as part of the service and target systems of the small spacecrafts are considered. It is shown how this can provide a significant increase in the tactical and technical characteristics of the small spacecrafts.
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