A Study of Air Launch Methods for RLVs

A Study of Air Launch Methods for RLVs
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RLV空中发射方法研究

DOI：
10.2514/6.2001-4619
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发表时间：
2001
期刊：
--
影响因子：
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通讯作者：
N. Sarigul
N. Sarigul
中科院分区：
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文献类型：
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作者：
M. Sarigul;N. Sarigul

文献摘要

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由于NASA的第二代空间发射倡议重新引起了人们的兴趣，许多组织提出了空中发射可重复使用的运载火箭(RLV)。空中发射的RLV分为顶部俘虏、底部俘虏、拖曳、空中加油和内部携带。评估了各种拟议的空中发射RLV概念的关键设计方面。人们发现，许多概念在当今的技术中是不可能的。作者介绍了一种新的空中发射概念，这种概念可以通过今天的技术称为SwiftLaunch RLV。
Many organizations have proposed air launch Reusable Launch Vehicles (RLVs) due to a renewed interest generated by NASA’s 2 Generation Space Launch Initiative. Air launched RLVs are categorized as captive on top, captive on bottom, towed, aerial refueled, and internally carried. The critical design aspects of various proposed air launch RLVs concepts are evaluated. It is found that many concepts are not possible with today’s technology. The authors introduce a new air launch concept that is possible with today’s technology called SwiftLaunch RLV.