RU96116785A - SOLID FUEL CHARGE FOR A ROCKET ENGINE WITH TWO OR MORE THROUGH STEPS - Google Patents

SOLID FUEL CHARGE FOR A ROCKET ENGINE WITH TWO OR MORE THROUGH STEPS

Info

Publication number
RU96116785A
RU96116785A RU96116785/06A RU96116785A RU96116785A RU 96116785 A RU96116785 A RU 96116785A RU 96116785/06 A RU96116785/06 A RU 96116785/06A RU 96116785 A RU96116785 A RU 96116785A RU 96116785 A RU96116785 A RU 96116785A
Authority
RU
Russia
Prior art keywords
solid fuel
rocket engine
steps
fuel charge
charge
Prior art date
Application number
RU96116785/06A
Other languages
Russian (ru)
Other versions
RU2131053C1 (en
Inventor
В.А. Дубинин
А.Н. Луговой
Д.Д. Аксененко
В.И. Марьяш
Е.П. Романов
Original Assignee
Научно-производственное объединение "Алтай"
Акционерная ассоциация "Атланта"
Filing date
Publication date
Application filed by Научно-производственное объединение "Алтай", Акционерная ассоциация "Атланта" filed Critical Научно-производственное объединение "Алтай"
Priority to RU96116785A priority Critical patent/RU2131053C1/en
Priority claimed from RU96116785A external-priority patent/RU2131053C1/en
Publication of RU96116785A publication Critical patent/RU96116785A/en
Application granted granted Critical
Publication of RU2131053C1 publication Critical patent/RU2131053C1/en

Links

Claims (1)

Заряд твердого топлива для ракетного двигателя с двумя или более ступенями тяги и разделительной перегородкой, состоящий по меньшей мере из двух газогенерирующих частей, отличающийся тем, что разделительная перегородка между его частями выполнена в виде шашки безгазового горения.The charge of solid fuel for a rocket engine with two or more stages of traction and a separation wall, consisting of at least two gas generating parts, characterized in that the separation wall between its parts is made in the form of gas-free combustion checkers.
RU96116785A 1996-08-15 1996-08-15 Solid propellant charge for dual thrust rocket engine RU2131053C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU96116785A RU2131053C1 (en) 1996-08-15 1996-08-15 Solid propellant charge for dual thrust rocket engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU96116785A RU2131053C1 (en) 1996-08-15 1996-08-15 Solid propellant charge for dual thrust rocket engine

Publications (2)

Publication Number Publication Date
RU96116785A true RU96116785A (en) 1998-11-20
RU2131053C1 RU2131053C1 (en) 1999-05-27

Family

ID=20184649

Family Applications (1)

Application Number Title Priority Date Filing Date
RU96116785A RU2131053C1 (en) 1996-08-15 1996-08-15 Solid propellant charge for dual thrust rocket engine

Country Status (1)

Country Link
RU (1) RU2131053C1 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2633976C1 (en) * 2016-06-09 2017-10-20 Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения имени П.И. Баранова" Solid fuel gas generator
CN113882969B (en) * 2021-09-30 2022-07-29 四川航天川南火工技术有限公司 Free-loading type single-chamber double-pushing solid small rocket structure

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