RU2013112428A - ON-BOARD COMMAND DEVICE ON THE ROCKET LAYOUT FOR PROCESSING THE START - Google Patents
ON-BOARD COMMAND DEVICE ON THE ROCKET LAYOUT FOR PROCESSING THE START Download PDFInfo
- Publication number
- RU2013112428A RU2013112428A RU2013112428/11A RU2013112428A RU2013112428A RU 2013112428 A RU2013112428 A RU 2013112428A RU 2013112428/11 A RU2013112428/11 A RU 2013112428/11A RU 2013112428 A RU2013112428 A RU 2013112428A RU 2013112428 A RU2013112428 A RU 2013112428A
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- Prior art keywords
- steering
- power source
- engine
- machines
- rocket
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- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
Бортовое командное устройство для отработки способа старта ракеты из пускового контейнера, с помощью пусков весогабаритного макета ракеты, имеющего, как на ракете, катапультирующее устройство (например, пороховой аккумулятор давления), двигатель первой ступени и рулевые машины органов управления, содержащие источник питания, электрически связанный с энергетическими средствами старта и рулевыми машинами, отличающееся тем, что в нем источник питания электрически связан с катапультирующим устройством, двигателем первой ступени и рулевыми машинами через установленные переключатели с нормально разомкнутыми контактами, на выходной электрической цепи источника питания использован переключатель, взаимодействующий с датчиком выхода макета, размещенным в районе верхнего торца пускового контейнера, в электрической цепи связи с двигателем установлен блок временной задержки его запуска относительно момента срабатывания датчика выхода, при подачи на рулевые машины электрического сигнала нужной полярности введены две параллельные цепи, в одной из которых подключен инвертор сигнала, а на штоках рулевых машин монтированы срезные штифты, первоначально удерживающие органы управления в нулевом положении, и механические ограничители их перемещения при дальнейшем движении макета.An on-board command device for practicing the method of launching a rocket from a launch container, using launches of a weight-sized missile model, having, like on a rocket, a catapult device (for example, a pressure powder accumulator), a first-stage engine and steering gears of controls containing a power source electrically connected with energy starting means and steering machines, characterized in that in it the power source is electrically connected to the ejection device, the engine of the first stage and the steering by machines through installed switches with normally open contacts, a switch is used on the output electrical circuit of the power source that interacts with the layout output sensor located in the region of the top end of the launch container, a block for the time delay of its launch relative to the moment the output sensor is triggered is installed in the electrical circuit for communication with the engine , when an electric signal of the required polarity is fed to the steering cars, two parallel circuits are introduced, in one of which an invert p signal, and on the rods of the steering machines mounted shear pins, initially holding the controls in the zero position, and mechanical stops for their movement during further movement of the layout.
Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2013112428/11A RU2536942C2 (en) | 2013-03-19 | 2013-03-19 | Onboard command device on missile dummy for take-off development |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2013112428/11A RU2536942C2 (en) | 2013-03-19 | 2013-03-19 | Onboard command device on missile dummy for take-off development |
Publications (2)
Publication Number | Publication Date |
---|---|
RU2013112428A true RU2013112428A (en) | 2014-09-27 |
RU2536942C2 RU2536942C2 (en) | 2014-12-27 |
Family
ID=51656282
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU2013112428/11A RU2536942C2 (en) | 2013-03-19 | 2013-03-19 | Onboard command device on missile dummy for take-off development |
Country Status (1)
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RU (1) | RU2536942C2 (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU171224U1 (en) * | 2016-12-15 | 2017-05-24 | Открытое акционерное общество "Научно-производственное предприятие "Звезда" имени академика Г.И. Северина" | Helicopter seat bailout control system |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7262395B2 (en) * | 2004-05-19 | 2007-08-28 | Derek Bilyk | Expendable sonobuoy flight kit with aerodynamically assisted sonobuoy separation |
US9004393B2 (en) * | 2010-10-24 | 2015-04-14 | University Of Kansas | Supersonic hovering air vehicle |
RU124247U1 (en) * | 2012-09-06 | 2013-01-20 | Открытое Акционерное Общество "Государственное Машиностроительное Конструкторское Бюро "Радуга" Имени А.Я. Березняка" | DEVICE FOR RESET USEFUL LOAD FROM AIRCRAFT (OPTIONS) |
RU124661U1 (en) * | 2012-09-20 | 2013-02-10 | Открытое Акционерное Общество "Государственное Машиностроительное Конструкторское Бюро "Радуга" Имени А.Я. Березняка" | DEVICE FOR RELEASING USEFUL LOADS FROM AIRCRAFT |
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2013
- 2013-03-19 RU RU2013112428/11A patent/RU2536942C2/en active
Also Published As
Publication number | Publication date |
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RU2536942C2 (en) | 2014-12-27 |
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Effective date: 20220224 |