RU96112436A - STAND FOR TESTS OF LIQUID ROCKET ENGINES - Google Patents

STAND FOR TESTS OF LIQUID ROCKET ENGINES

Info

Publication number
RU96112436A
RU96112436A RU96112436/06A RU96112436A RU96112436A RU 96112436 A RU96112436 A RU 96112436A RU 96112436/06 A RU96112436/06 A RU 96112436/06A RU 96112436 A RU96112436 A RU 96112436A RU 96112436 A RU96112436 A RU 96112436A
Authority
RU
Russia
Prior art keywords
tanks
lines
valves
rocket engines
separation
Prior art date
Application number
RU96112436/06A
Other languages
Russian (ru)
Other versions
RU2111373C1 (en
Inventor
Л.Д. Круцких
А.С. Микиша
В.И. Полиенко
Original Assignee
Конструкторское бюро химавтоматики
Filing date
Publication date
Application filed by Конструкторское бюро химавтоматики filed Critical Конструкторское бюро химавтоматики
Priority to RU96112436A priority Critical patent/RU2111373C1/en
Priority claimed from RU96112436A external-priority patent/RU2111373C1/en
Application granted granted Critical
Publication of RU2111373C1 publication Critical patent/RU2111373C1/en
Publication of RU96112436A publication Critical patent/RU96112436A/en

Links

Claims (1)

Стенд для испытаний жидкостных ракетных двигателей, содержащий системы подачи компонентов топлива к двигателю, включающие в себя расходные баки, разделительные и бустерные емкости, расходные магистрали с расходомерами, пусковые магистрали, топливную арматуру, магистрали сжатых газов, отличающийся тем, что в нем в разделительные емкости установлены отсечные клапаны с седлами, герметично соединенными с входами пусковых магистралей, а снаружи разделительных емкостей установлены приводы клапанов, причем клапаны и их приводы соединены между собой механическими связями, которые проходят через отверстия с уплотнениями в стенках разделительных емкостей.A test bench for liquid-propellant rocket engines, containing systems for supplying fuel components to the engine, including supply tanks, separation and booster tanks, supply lines with flow meters, starting lines, fuel valves, compressed gas lines, characterized in that it contains separation tanks shut-off valves are installed with seats that are hermetically connected to the inputs of the launch lines, and valve actuators are installed outside the separation tanks, and the valves and their actuators are connected Do a mechanical linkages which extend through openings with seals in the walls separating the tanks.
RU96112436A 1996-06-18 1996-06-18 Liquid-propellant rocket engine test stand RU2111373C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU96112436A RU2111373C1 (en) 1996-06-18 1996-06-18 Liquid-propellant rocket engine test stand

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU96112436A RU2111373C1 (en) 1996-06-18 1996-06-18 Liquid-propellant rocket engine test stand

Publications (2)

Publication Number Publication Date
RU2111373C1 RU2111373C1 (en) 1998-05-20
RU96112436A true RU96112436A (en) 1998-08-27

Family

ID=20182167

Family Applications (1)

Application Number Title Priority Date Filing Date
RU96112436A RU2111373C1 (en) 1996-06-18 1996-06-18 Liquid-propellant rocket engine test stand

Country Status (1)

Country Link
RU (1) RU2111373C1 (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2445503C1 (en) * 2010-10-08 2012-03-20 Открытое акционерное общество "Конструкторское бюро химавтоматики" Test bench for testing power plants with fuel cryogenic components
RU2611119C1 (en) * 2015-10-14 2017-02-21 Акционерное общество "Конструкторское бюро химавтоматики" Stand for power plants with used process gas accumulation testing
RU2631371C1 (en) * 2016-05-23 2017-09-21 Акционерное общество "Конструкторское бюро химавтоматики" Power installation test method and test bench for its implementation
RU2770072C2 (en) * 2021-06-09 2022-04-14 Валентин Павлович Рылов Test bench for the pumping system for powdered metal supply to the combustion chamber of a rocket engine

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