纳米卫星混合空射火箭初步设计

2007 International Conference on Computational Science and its Applications (ICCSA 2007) Pub Date : 2007-08-26 DOI:10.1109/ICCSA.2007.16

Jae-Woo Lee, K. Noh, Y. Byun, Bong-Kyo Park

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引用次数: 10

摘要

空中发射是发射“纳米卫星”的一种有效方法，发射成本低。本文对空射微型火箭进行了初步设计。在此基础上进行了任务和弹道优化，并设计了推进系统。设计了总重量为830.95 kg、有效载荷为3.56 kg、推进系统长度为5.89 m的超音速空射火箭。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

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Preliminary Design of the Hybrid Air-launching Rocket for Nanosat

Air-Launching is an effective method that can launch the 'Nanosat' for low launching cost. In this study, the preliminary design of the air-launching micro rocket was performed. Mission and trajectory optimization was performed and the propulsion system was designed based on the mission design. A supersonic air launching rocket with total weight of 830.95 kg, the payload weight of 3.56 kg and the propulsion system length of 5.89 m has been designed.

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2007 International Conference on Computational Science and its Applications (ICCSA 2007)

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