FIELD: rocket equipment.
SUBSTANCE: invention can be used in structures of sustainer stages of rocket engines of solid fuel. Engine comprises a combustion chamber having a cylindrical section, a front and a rear bottoms, a nozzle with a recessed portion, a charge attached to the combustion chamber, igniter and, unlike the prototype, is equipped with a profiled hollow insert located inside the combustion chamber coaxially to the nozzle at the specified distance from it.
EFFECT: engine has a simpler design, which reduces engine cost, and also ensures stable operation of the engine at almost maximum value of its power.
1 cl, 1 dwg
Title |
Year |
Author |
Number |
SOLID-PROPELLANT ROCKET ENGINE WITH TURNING CONTROL NOZZLE (VERSIONS) |
2010 |
- Gubertov Arnol'D Mikhajlovich
- Mironov Vadim Vsevolodovich
- Davydenko Nikolaj Andreevich
- Borisov Dmitrij Marianovich
- Ul'Janova Marina Viktorovna
- Degtjarev Sergej Antonovich
|
RU2428579C1 |
SOLID-PROPELLANT ROCKET ENGINE (VERSIONS) |
2009 |
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- Mironov Vadim Vsevolodovich
- Davydenko Nikolaj Andreevich
- Borisov Dmitrij Marianovich
- Kuranov Mikhail Leonidovich
- Ul'Janova Marina Viktorovna
- Degtjarev Sergej Antonovich
|
RU2429368C1 |
NOZZLE-FREE SOLID-PROPELLANT ROCKET ENGINE |
2012 |
- Gubertov Arnol'D Mikhajlovich
- Mironov Vadim Vsevolodovich
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- Borisov Dmitrij Marianovich
- Ul'Janova Marina Viktorovna
- Degtjarev Sergej Antonovich
|
RU2517971C1 |
SOLID-PROPELLANT ROCKET ENGINE |
2002 |
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- Molchanov V.F.
- Pribyl'Skij R.E.
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- Fedorov S.T.
- Fedchenko N.N.
- Renskov A.P.
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2005 |
- Raimov Rinat Khamidovich
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- Nikitin Vasilij Tikhonovich
- Koz'Jakov Aleksej Vasil'Evich
- Molchanov Vladimir Fedorovich
- Magsumov Nail' Nazipovich
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|
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2012 |
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|
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2003 |
- Gubertov A.M.
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- Gollender R.G.
- Trusov Ju.D.
|
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2006 |
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2006 |
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|
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2012 |
- Molchanov Vladimir Fedorovich
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- Krasil'Nikov Fedor Sergeevich
- Zakirova Ol'Ga Viktorovna
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|
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