Problems and ways of their solutions in the development of a lowthrust liquid jet engine for a stage 3 liquid jet system of «Cyclone-4» launch vehicle-Reference-Cited by-同舟云学术

Problems and ways of their solutions in the development of a lowthrust liquid jet engine for a stage 3 liquid jet system of «Cyclone-4» launch vehicle

Published:2020 Issue:1 Volume:26 Page:18-29
ISSN:1561-8889
Container-title:Kosmìčna nauka ì tehnologìâ
language:
Short-container-title:Kosm. nauka tehnol.

Author:

Durachenko V.M., ,Shpak A.V.,Kolesnychenko S.A.,Aheyeva L.I.,Dolinkevich A.S.,Unchur K.O., , , , ,

Publisher

National Academy of Sciences of Ukraine (Co. LTD Ukrinformnauka)

Subject

Anesthesiology and Pain Medicine

Reference9 articles.

1. 1. Abramovich G. (1969). Applied gas dynamics. Moscow.

2. 2. Belyaiev N., Belik N., Uvarov Y. (1979). Spacecraft jet control systems. Moscow: Machinebuilding,

3. 3. Vasiliev A., Kudryavtsev V., Kuznetsov A. (1975). Basis of liquid-propellant rocket engine theory and calculation. Moscow.

4. 4. Deitch M. (1961). Technical gas dynamics. Moscow.

5. 5. Yegorychev V. (2014). Liquid-propellant rocket thrusters and their characteristics. Samara.

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