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Construction and design of LPRE units. Chambers
Uploaded: 27.07.2018
Content: construction_[RocketEngines.ru].pdf 2377,98 kB
Product description
The questions of designing and designing of the most heat-stressed unit of the propulsion system - the chamber of the liquid rocket engine are described. Various calculation methods, a large amount of reference materials and examples of the constructive solution necessary for the design are given.
For students of senior courses of higher educational institutions. It can be used in practical work by engineers engaged in the development of liquid rocket engine cameras for various purposes.
Additional information
D.I. Zawistovskiy, V.V. Spesivtsev
Construction and design of liquid propellant rocket engines assemblies. Chambers
Tutorial. – Kharkov: National aerospace university «Kharkov aviation institute», 2003. – 122 p.
Il. 87, Tabl. 14, Bibliogr.: 20 titles.
Edition 2, revised, 2008
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