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    Please use this identifier to cite or link to this item: http://ir.lib.ncu.edu.tw/handle/987654321/30682


    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:[機械工程研究所] 期刊論文

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