A concept of vertical takeoff two-stage-to-orbit reusable launch vehicle with an Integral-Rocket-Ramjet booster

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Title:	A concept of vertical takeoff two-stage-to-orbit reusable launch vehicle with an Integral-Rocket-Ramjet booster
Authors:	Hong,ZC;Lee,CC;Tseng,CJ
Contributors:	機械工程研究所
Date:	2005
Issue Date:	2010-07-06 16:24:58 (UTC+8)
Publisher:	中央大學
Abstract:	Reusable launch vehicles (RLV) currently envisioned incorporate a Aide variety of propulsion types. Various propulsion devices have been designed, or are being designed. The Integral-Rocket-Ranijet (IRR) propulsion mainly applies to a tactical missile boo
Relation:	JOURNAL OF MECHANICS
Appears in Collections:	[Graduate Institute of Mechanical Engineering] journal & Dissertation

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