ROCKET ENGINE Russian patent published in 2014 - IPC F02K9/70 

Abstract RU 2526000 C1

FIELD: engines and pumps.

SUBSTANCE: proposed engine comprises body, charge composed of solid pasty propellants and plugs preventing pasty propellant from bleeding. Solid propellant charge has lengthwise and crosswise dead channels partially coated with adhesive composition and extending over to solid-propellant charge surface. Dead channels are filled with pasty propellant and stopped on the side of solid-propellant charge by plugs of quick-combustible material.

EFFECT: higher propellant filling ratio, invariable shape of the charge.

7 cl, 3 dwg

Similar patents RU2526000C1

Title Year Author Number
SOLID PROPELLANT ROCKET ENGINE 2013
  • Zharkov Aleksandr Sergeevich
  • Dochilov Nikolaj Egorovich
  • Gromov Aleksandr Mikhajlovich
  • Kazakov Aleksandr Alekseevich
RU2527280C1
REACTIVE METAL DEVICE 2018
  • Prudnikov Aleksandr Grigorevich
  • Lanshin Aleksandr Igorevich
  • Severinova Viktoriya Viktorovna
  • Podvalnyj Artem Mikhajlovich
  • Roshchin Aleksandr Viktorovich
  • Bloshenko Aleksandr Vitalevich
RU2680568C1
SOLID-PROPELLANT ROCKET ENGINE (VERSIONS) 2016
  • Glebov Gennadij Aleksandrovich
  • Abdrakhmanov Farid Khabibullovich
  • Ershov Anatolij Mikhajlovich
  • Kojtov Stanislav Anatolevich
RU2642764C2
SOLID-PROPELLANT ROCKET ENGINE 2010
  • Sidorov Pavel Mikhajlovich
  • Kurganov Oleg Borisovich
  • Krasnova Galina Petrovna
RU2422663C1
STAROVEROV'S CONICAL ROCKET ENGINE 8 (VERSIONS) AND METHOD OF ITS VERTICAL LAUNCHING (VERSIONS) 2013
  • Staroverov Nikolaj Evgen'Evich
RU2524793C1
ROCKET ENGINE OF ROCKET-ASSISTED PROJECTILE 2016
  • Arkhipov Vladimir Afanasevich
  • Konovalenko Aleksej Ivanovich
  • Perfileva Kseniya Grigorevna
  • Zhukov Aleksandr Stepanovich
  • Bondarchuk Sergej Sergeevich
RU2620613C1
SOLID-PROPELLANT ROCKET ENGINE FOR GUIDED PROJECTILE AND SOLID PROPELLANT IGNITOR 1994
  • Glukharev N.N.
  • Andreev V.A.
  • Aleshichev I.A.
  • Dronov E.A.
  • Sokolova M.N.
RU2079689C1
SOLID-FUEL ROCKET ENGINE OF GUIDED PROJECTILE 2015
RU2613351C1
PYROTECHNIC TRAIN-TYPE IGNITION SYSTEM 2000
  • Lukin A.N.
RU2178093C2
STAROVERV'S-8 ROCKET ENGINE (VERSIONS) 2012
  • Staroverov Nikolaj Evgen'Evich
RU2561820C2

RU 2 526 000 C1

Authors

Zharkov Aleksandr Sergeevich

Dochilov Nikolaj Egorovich

Kazakov Aleksandr Alekseevich

Kalmykov Petr Ivanovich

Shatnyj Mikhail Vasil'Evich

Nesterov Grigorij Nikolaevich

Sakovich Gennadij Viktorovich

Dates

2014-08-20Published

2013-01-10Filed