RU99105957A - CONTROLLED ROCKET ENGINE - Google Patents

CONTROLLED ROCKET ENGINE

Info

Publication number
RU99105957A
RU99105957A RU99105957/06A RU99105957A RU99105957A RU 99105957 A RU99105957 A RU 99105957A RU 99105957/06 A RU99105957/06 A RU 99105957/06A RU 99105957 A RU99105957 A RU 99105957A RU 99105957 A RU99105957 A RU 99105957A
Authority
RU
Russia
Prior art keywords
nozzle
cavity
rocket engine
unit
housing
Prior art date
Application number
RU99105957/06A
Other languages
Russian (ru)
Other versions
RU2171389C2 (en
Inventor
Михаил Иванович Соколовский
Сергей Викторович Лянгузов
Сергей Витальевич Огнев
Original Assignee
Открытое акционерное общество Научно-производственное объединение "Искра"
Filing date
Publication date
Application filed by Открытое акционерное общество Научно-производственное объединение "Искра" filed Critical Открытое акционерное общество Научно-производственное объединение "Искра"
Priority to RU99105957A priority Critical patent/RU2171389C2/en
Priority claimed from RU99105957A external-priority patent/RU2171389C2/en
Publication of RU99105957A publication Critical patent/RU99105957A/en
Application granted granted Critical
Publication of RU2171389C2 publication Critical patent/RU2171389C2/en

Links

Claims (1)

Управляемый ракетный двигатель, содержащий корпус, заряд, сопло и гидравлический узел, состоящий из обращенного в полость корпуса стакана, установленного в стакане с возможностью продольного перемещения дифференциального поршня, жидкости, находящейся в подпоршневой полости стакана, причем подпоршневая полость стакана через регулируемый дроссель связана с форсуночным блоком, отличающийся тем, что форсуночный блок обращен в полость корпуса, а жидкостью, находящейся в подпоршневой полости стакана является хладагент (например, вода).A guided rocket engine comprising a housing, a charge, a nozzle, and a hydraulic unit, consisting of a nozzle facing the cavity of the nozzle installed in the nozzle with the possibility of longitudinal movement of the differential piston, fluid located in the nozzle cavity of the nozzle, the nozzle cavity of the nozzle connected via an adjustable throttle to the nozzle unit, characterized in that the nozzle unit is facing the cavity of the housing, and the liquid located in the sub-piston cavity of the glass is a refrigerant (for example, water).
RU99105957A 1999-03-23 1999-03-23 Controlled rocket engine RU2171389C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU99105957A RU2171389C2 (en) 1999-03-23 1999-03-23 Controlled rocket engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU99105957A RU2171389C2 (en) 1999-03-23 1999-03-23 Controlled rocket engine

Publications (2)

Publication Number Publication Date
RU99105957A true RU99105957A (en) 2001-01-20
RU2171389C2 RU2171389C2 (en) 2001-07-27

Family

ID=20217551

Family Applications (1)

Application Number Title Priority Date Filing Date
RU99105957A RU2171389C2 (en) 1999-03-23 1999-03-23 Controlled rocket engine

Country Status (1)

Country Link
RU (1) RU2171389C2 (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8352099B1 (en) * 2009-07-09 2013-01-08 The Boeing Company Varying engine thrust for directional control of an aircraft experiencing engine thrust asymmetry
RU2477810C1 (en) * 2011-08-05 2013-03-20 Открытое акционерное общество "ФНПЦ "Алтай" Method for damping of operating solid-propellant rocket engine during tests, and plant for its implementation
RU2527228C1 (en) * 2013-02-19 2014-08-27 Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Тульский государственный университет" (ТулГУ) Solid-propellant engine nozzle unit
RU2633976C1 (en) * 2016-06-09 2017-10-20 Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения имени П.И. Баранова" Solid fuel gas generator

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