Thermo Structural Analysis of Carbon-Carbon Nozzle Exit Cone for Rocket Cryo Engines

Publisher: Trans Tech Publications

E-ISSN: 1662-7482|2018|877|320-326

ISSN: 1660-9336

Source: Applied Mechanics and Materials, Vol.2018, Iss.877, 2018-03, pp. : 320-326

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Abstract