Design aspects of launch vehicle sizing including air-breathing propulsion

Abstract The overall sizing of launch vehicles is of interest, especially when air-breathing is also included. The sizing of a launch vehicle is dictated by the State of Art technologies present and the need to match the challenging demands of high-payload fraction, low cost, and also ensure reliabi...

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Veröffentlicht in:	Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering Journal of aerospace engineering, 2006-10, Vol.220 (5), p.487-498
1. Verfasser:	Sundaresan, M
Format:	Artikel
Sprache:	eng
Schlagworte:	Design engineering Flight simulation Spacecraft
Online-Zugang:	Volltext
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