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DEVELOPMENT OF ILR-33 AMBER SOUNDING ROCKET FOR MICROGRAVITY EXPERIMENTS

机译:用于微重力实验的ILR-33琥珀色测深火箭的研制

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This paper gives an overview of the development of ILR-33 Amber sounding rocket designated for microgravity experiments, that was performed in Institute of Aviation in Warsaw, Poland. The lack of easy accessible and affordable platform for this kind of research was one of the key reasons for this work. Proposed design enables to perform experiments in microgravity for almost 150 seconds with apogee over 100 km. Combining this results with relatively low price per launch and short deployment time gives firm position on the market. The paper covers different type of payload considerations and cost analyses. This article describes also rocket design and its capabilities. Proposed design utilizes hybrid type of rocket motor with High Test Peroxide as an oxidizer along with two reusable solid rocket boosters. The early phase analysis of the rocket configuration and propellant considerations are also presented in the paper. Furthermore already performed testing phase including: wind tunnel research, motors design, manufacture and tests and drop down tests is also covered in this article. The proposed design is also considered as introduction phase for small rocket launcher that could deliver pico and nanosatellites to LEO orbits. This solution is described by the possibility of rocket air-platform launch.
机译:本文概述了用于微重力实验的ILR-33琥珀探测火箭的发展,该火箭是在波兰华沙的航空研究所进行的。缺乏此类研究的便捷,负担得起的平台是这项工作的主要原因之一。拟议的设计使远地点超过100公里,可以在微重力下进行近150秒的实验。将这些结果与相对较低的每次发射价格和较短的部署时间相结合,可以在市场上占据稳固的位置。本文涵盖了不同类型的有效载荷注意事项和成本分析。本文还介绍了火箭的设计及其功能。拟议的设计将混合型火箭发动机与高测试过氧化物用作氧化剂,并使用两个可重复使用的固体火箭助推器。本文还介绍了火箭构型的早期分析和推进剂的注意事项。此外,本文还介绍了已经执行的测试阶段,包括:风洞研究,电机设计,制造和测试以及跌落测试。拟议的设计也被认为是小型火箭发射器的引入阶段,可以将微微和纳米卫星传送到LEO轨道。该解决方案通过火箭空中平台发射的可能性来描述。

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