A Concept of Vertical Takeoff Two-Stage-to-Orbit Reusable Launch Vehicle with an Integral-Rocket-Ramjet Booster

Publisher： Cambridge University Press

E-ISSN： 1811-8216|21|1|51-56

ISSN： 1727-7191

Source： Journal of Mechanics, Vol.21, Iss.1, 2005-03, pp. : 51-56

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