RU2000104196A - ROCKET AND RECTIFIER ENGINE - Google Patents

ROCKET AND RECTIFIER ENGINE

Info

Publication number
RU2000104196A
RU2000104196A RU2000104196/06A RU2000104196A RU2000104196A RU 2000104196 A RU2000104196 A RU 2000104196A RU 2000104196/06 A RU2000104196/06 A RU 2000104196/06A RU 2000104196 A RU2000104196 A RU 2000104196A RU 2000104196 A RU2000104196 A RU 2000104196A
Authority
RU
Russia
Prior art keywords
engine
rocket
rectifier
afterburner
gas generator
Prior art date
Application number
RU2000104196/06A
Other languages
Russian (ru)
Other versions
RU2195566C2 (en
Inventor
Иван Николаевич Лазовик
Сергей Александрович Морозов
Александр Владимирович Подкопаев
Original Assignee
Иркутский военный авиационный инженерный институт
Filing date
Publication date
Application filed by Иркутский военный авиационный инженерный институт filed Critical Иркутский военный авиационный инженерный институт
Priority to RU2000104196A priority Critical patent/RU2195566C2/en
Priority claimed from RU2000104196A external-priority patent/RU2195566C2/en
Publication of RU2000104196A publication Critical patent/RU2000104196A/en
Application granted granted Critical
Publication of RU2195566C2 publication Critical patent/RU2195566C2/en

Links

Claims (1)

Ракетно-прямоточный двигатель, содержащий камеру дожигания с соплом Лаваля, газогенератор, заряд твердого топлива, воспламенитель, воздухозаборник, отличающийся тем, что вращающийся газогенератор находится внутри камеры дожигания и имеет полупетлевые сопла, размещенные под углом в 20-30o к оси двигателя.A ramjet engine containing an afterburner with a Laval nozzle, a gas generator, a solid fuel charge, an ignitor, an air intake, characterized in that the rotating gas generator is located inside the afterburner and has half-loop nozzles placed at an angle of 20-30 o to the axis of the engine.
RU2000104196A 2000-02-21 2000-02-21 Rocket ramjet engine RU2195566C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2000104196A RU2195566C2 (en) 2000-02-21 2000-02-21 Rocket ramjet engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2000104196A RU2195566C2 (en) 2000-02-21 2000-02-21 Rocket ramjet engine

Publications (2)

Publication Number Publication Date
RU2000104196A true RU2000104196A (en) 2002-01-20
RU2195566C2 RU2195566C2 (en) 2002-12-27

Family

ID=20230881

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2000104196A RU2195566C2 (en) 2000-02-21 2000-02-21 Rocket ramjet engine

Country Status (1)

Country Link
RU (1) RU2195566C2 (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2615889C1 (en) * 2015-11-19 2017-04-11 Российская Федерация, от имени которой выступает Государственная корпорация по космической деятельности "РОСКОСМОС" Rocket-ramjet engine with adjustable flow rate of solid fuel
RU180227U1 (en) * 2017-11-02 2018-06-06 Закрытое акционерное общество "Институт телекоммуникаций" Combined three-mode jet engine
CN109630315B (en) * 2019-02-25 2020-06-16 中国人民解放军国防科技大学 Solid rocket scramjet engine, arc-shaped gas generator and central injection device
CN110700963B (en) * 2019-08-15 2021-03-02 西北工业大学 Compact layout type solid rocket gas scramjet engine based on axial symmetry

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