Feasibility of a low-cost sounding rockoon platform
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- 作者：Adam Okninskia ; adam.okninski@ilot.edu.pl" class="auth_mail" title="E-mail the corresponding authorAuthor Vitae ; Daniel Sors RaurellbAuthor Vitae ; Alberto Rodriguez MitrebAuthor Vitae
- 关键词：AP ; Ammonium Perchlorate ; CFRP ; Carbon Fiber Reinforced Plastic ; COTS ; Commercially-of-the-Shelf ; DLR ; Deutsches Zentrum fü ; r Luft- und Raumfahrt (English ; German Aerospace Center) ; HTPB ; Hydroxyl-Terminated Polybutadiene ; LEEM ; Laboratory for Space and Microgravity Research ; SL ; Sea Level ; SRM ; Solid Rocket Motor ; SSRP ; Small Sounding Rocket Program ; WUT ; Warsaw University of Technology.
- 刊名：Acta Astronautica
- 出版年：2016
- 出版时间：October-November 2016
- 年：2016
- 卷：127
- 期：Complete
- 页码：335-344
- 全文大小：1501 K
文摘
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Sounding rocket systems using a balloon-platform first stage are considered for low-cost in-flight experimentation.
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A preliminary design to enable delivering 1 kg payloads to over 100 km is outlined.
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Special attention is given to the propulsion system, which is based on a solid rocket motor.
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The influence of key vehicle design parameters on system performance was investigated.
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System mass and cost optimization was performed.