FIELD: rocket technology.
SUBSTANCE: rocket contains a head part, a rocket part, a nozzle block, including a nozzle, a liner, and a base with blades. According to the invention, the nozzle is equipped with a cylindrical section, the diameter of which (D1) in the cross-section passing through the nozzle exit section is (0.85- 0.97), and its width (h), respectively, is (0.04-0.22) of the diameter of the rocket, and the outer diameter of the base (D2) is (0.88-0.999) of the outer diameter of the nozzle in the cross-section passing through the nozzle exit section.
EFFECT: improved reliability of the rocket in the process of leaving the guide.
2 cl, 2 dwg
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Year |
Author |
Number |
| MISSILE PART WITH STABILISER OF ROCKET PROJECTILE |
2014 |
- Makarovets Nikolaj Aleksandrovich
- Aljazhedinov Vadim Rashitovich
- Tregubov Viktor Ivanovich
- Verbovenko Aleksandr Andreevich
- Kashirkin Aleksandr Aleksandrovich
- Bazarnyj Aleksej Nikolaevich
- Erokhin Vladimir Evgen'Evich
- Zakharov Sergej Olegovich
|
RU2540291C1 |
| ROCKET PROJECTILE LAUNCHED FROM LAUNCHING TUBE |
1997 |
- Belobragin V.N.
- Denezhkin G.A.
- Kuksenko A.F.
- Makarovets N.A.
- Mar'In V.V.
- Medvedev V.I.
- Podchufarov V.I.
- Proskurin N.M.
- Romanovtsev B.M.
- Abramov N.V.
- Sopikov D.V.
- Kaljuzhnyj G.V.
- Semilet V.V.
- Kobylin R.A.
|
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| ROCKET PROJECTILE WITH A GAS-DYNAMIC STABILIZATION SYSTEM |
2020 |
- Alyazhedinov Vadim Rashitovich
- Belobragin Boris Andreevich
- Zakharov Oleg Lvovich
- Bazarnyj Aleksej Nikolaevich
- Tregubov Viktor Ivanovich
- Zakharov Sergej Olegovich
- Popov Sergej Viktorovich
- Borisov Oleg Grigorevich
- Erokhin Vladimir Viktorovich
|
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| ROCKET PART OF MISSILE FIRED FROM TUBULAR GUIDE |
2023 |
- Astashov Vladislav Sergeevich
- Belobragin Boris Andreevich
- Borisov Oleg Grigorevich
- Evlanov Andrej Aleksandrovich
- Popov Sergej Viktorovich
- Zakharov Sergej Olegovich
- Khlebnikov Igor Ivanovich
|
RU2808543C1 |
| JET PROJECTILE ROCKET SECTION |
2014 |
- Makarovets Nikolaj Aleksandrovich
- Denezhkin Gennadij Alekseevich
- Belobragin Boris Andreevich
- Druzhinin Vladimir Evgen'Evich
- Filippov Vladimir Sergeevich
- Kazakov Konstantin Igorevich
- Verkin Jurij Petrovich
- Koloskov Boris Petrovich
- Terekhova Ol'Ga Anatol'Evna
|
RU2559657C1 |
| SOLID-PROPELLANT ROCKET ENGINE |
2023 |
- Belobragin Boris Andreevich
- Erokhin Vladimir Viktorovich
- Zakharov Sergej Olegovich
- Evlanov Andrej Aleksandrovich
- Vlasov Aleksej Vladimirovich
- Khlebnikov Igor Ivanovich
- Medvedev Vladimir Ivanovich
|
RU2816347C1 |
| ROCKET ENGINE SEALING STARTER |
2013 |
- Makarovets Nikolaj Aleksandrovich
- Zakharov Oleg L'Vovich
- Kashirkin Aleksandr Aleksandrovich
- Bazarnyj Aleksej Nikolaevich
- Erokhin Vladimir Evgen'Evich
- Medvedev Vladimir Ivanovich
|
RU2524785C1 |
| ROTATING MISSILE |
2020 |
- Alyazhedinov Vadim Rashitovich
- Belobragin Boris Andreevich
- Tregubov Viktor Ivanovich
- Bazarnyj Aleksej Nikolaevich
- Medvedev Vladimir Ivanovich
- Khlebnikov Igor Ivanovich
- Zakharov Oleg Lvovich
- Zakharov Sergej Olegovich
- Erokhin Vladimir Evgenevich
- Kuznetsov Vitalij Vasilevich
- Bykonya Igor Petrovich
- Mikhajlov Andrej Vladimirovich
- Khrykov Viktor Viktorovich
- Shatunova Natalya Nikolaevna
|
RU2732370C1 |
| ROCKET SECTION WITH STABILISING DEVICE OF PROJECTILE |
2015 |
- Makarovets Nikolaj Aleksandrovich
- Tregubov Viktor Ivanovich
- Verbovenko Aleksandr Andreevich
- Ivanov Igor Vladimirovich
- Zakharov Sergej Olegovich
- Bazarnyj Aleksej Nikolaevich
- Erokhin Vladimir Evgenevich
- Kazarinov Leonid Dmitrievich
|
RU2581097C1 |
| ROTARY JET PROJECTILE |
2011 |
- Makarovets Nikolaj Aleksandrovich
- Kaljuzhnyj Gennadij Vasil'Evich
- Denezhkin Gennadij Alekseevich
- Zakharov Oleg L'Vovich
- Medvedev Vladimir Ivanovich
- Kuksenko Aleksandr Fedorovich
- Bazarnyj Aleksej Nikolaevich
- Zakharov Sergej Olegovich
|
RU2451902C1 |
