FIELD: rocket technology.
SUBSTANCE: rocket part containing a block of stabilizers, blades, a base with grooves on a cylindrical surface for fixing the blades, a nozzle including inlet and outlet cones, according to the invention, with one or more drainage holes on the base located at a distance of (0.001…0.08) of the length of the base (Lbase) from the end of the base, the total area of which is (0.001…0.017) of the surface area of the nozzle exit cone under the base.
EFFECT: invention improves the reliability of the functioning of a rocket unit using high-energy fuels due to the effective cooling of the nozzle exit cone.
1 cl, 1 dwg
| Title |
Year |
Author |
Number |
| ROCKET PART OF MISSILE FIRED FROM TUBULAR GUIDE |
2023 |
- Belobragin Boris Andreevich
- Babin Sergej Aleksandrovich
- Zakharov Sergej Olegovich
- Evlanov Andrej Aleksandrovich
- Vlasov Aleksej Vladimirovich
- Khlebnikov Igor Ivanovich
- Medvedev Vladimir Ivanovich
|
RU2808695C1 |
| ROCKET PROJECTILE LAUNCHED FROM TUBULAR GUIDE |
2023 |
- Belobragin Boris Andreevich
- Erokhin Vladimir Viktorovich
- Zakharov Sergej Olegovich
- Evlanov Andrej Aleksandrovich
- Vlasov Aleksej Vladimirovich
- Khlebnikov Igor Ivanovich
- Borisov Oleg Grigorevich
- Medvedev Vladimir Ivanovich
- Erokhin Vladimir Evgenevich
- Tregubov Viktor Ivanovich
|
RU2806232C1 |
| MISSILE PART OF A ROTATING ROCKET PROJECTILE LAUNCHED FROM A SMOOTHBORE TUBULAR GUIDE |
2022 |
- Belobragin Boris Andreevich
- Babin Sergej Aleksandrovich
- Zakharov Sergej Olegovich
- Medvedev Vladimir Ivanovich
- Evlanov Andrej Aleksandrovich
- Vlasov Aleksej Vladimirovich
- Zotov Vladimir Nikolaevich
- Smirnov Aleksandr Vladimirovich
|
RU2798116C1 |
| MISSILE |
2016 |
- Tregubov Viktor Ivanovich
- Zakharov Oleg Lvovich
- Bazarnyj Aleksej Nikolaevich
- Medvedev Vladimir Ivanovich
- Erokhin Vladimir Evgenevich
- Kashirkin Aleksandr Aleksandrovich
- Kuznetsov Vitalij Vasilevich
- Bykonya Igor Petrovich
- Bondarenko Tatyana Petrovna
|
RU2623373C1 |
| ROCKET |
1998 |
- Belobragin V.N.
- Gromov N.I.
- Gushchin V.A.
- Denezhkin G.A.
- Makarovets N.A.
- Obozov L.I.
- Petrov V.L.
- Podchufarov V.I.
- Semilet V.V.
|
RU2125701C1 |
| NOZZLE UNIT OF SOLID-PROPELLANT ROCKER ENGINE WITH FITTED-ON STABILIZER UNIT |
2001 |
- Makarovets N.A.
- Denezhkin G.A.
- Semilet V.V.
- Kashirkin A.A.
- Peturkin D.M.
- Filatov V.G.
- Prolubnikov V.I.
- Bendrikovskij P.V.
|
RU2179651C1 |
| 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 ENGINE OF ROCKET-ASSISTED PROJECTILE |
2016 |
- Arkhipov Vladimir Afanasevich
- Konovalenko Aleksej Ivanovich
- Perfileva Kseniya Grigorevna
- Zhukov Aleksandr Stepanovich
- Bondarchuk Sergej Sergeevich
|
RU2620613C1 |
| 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 |
| JET PROJECTILE LAUNCHED FROM LAUNCHING TUBE |
2000 |
- Belobragin V.N.
- Verbovenko A.A.
- Darovskij V.A.
- Denezhkin G.A.
- Evtukhov E.I.
- Nosov L.S.
- Kashirkin A.A.
- Kuksenko A.F.
- Makarovets N.A.
- Obozov L.I.
- Podchufarov V.I.
- Semilet V.V.
- Belobragin B.A.
|
RU2176068C1 |
