RU2006132135A - MODEL ROCKET COMPLEX - Google Patents

MODEL ROCKET COMPLEX Download PDF

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Publication number
RU2006132135A
RU2006132135A RU2006132135/12A RU2006132135A RU2006132135A RU 2006132135 A RU2006132135 A RU 2006132135A RU 2006132135/12 A RU2006132135/12 A RU 2006132135/12A RU 2006132135 A RU2006132135 A RU 2006132135A RU 2006132135 A RU2006132135 A RU 2006132135A
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RU
Russia
Prior art keywords
rocket
complex according
launch
nozzle
model
Prior art date
Application number
RU2006132135/12A
Other languages
Russian (ru)
Other versions
RU2328330C1 (en
Inventor
Михаил Михайлович Козырь (RU)
Михаил Михайлович Козырь
Original Assignee
Михаил Михайлович Козырь (RU)
Михаил Михайлович Козырь
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Михаил Михайлович Козырь (RU), Михаил Михайлович Козырь filed Critical Михаил Михайлович Козырь (RU)
Priority to RU2006132135/12A priority Critical patent/RU2328330C1/en
Publication of RU2006132135A publication Critical patent/RU2006132135A/en
Application granted granted Critical
Publication of RU2328330C1 publication Critical patent/RU2328330C1/en

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Claims (6)

1. Модельный ракетный комплекс, содержащий основание со складывающимися опорами и стойкой, на которой установлены модельная ракета, средства ее удержания, наведения и дистанционного управления пуском, отличающийся тем, что пусковое устройство содержит: предохранитель от самопроизвольного пуска ракеты, захваты на шарнирах, ползун клинообразной формы для удержания ракеты и пружину растяжения для отвода захватов при запуске, воздухопровод с ниппелем для подачи сжатого воздуха в корпус-двигатель, а на корпусе пускового устройства имеется паз для крепления его винтом к направляющей консоли.1. A model missile system containing a base with folding supports and a rack on which a model rocket is mounted, means for holding it, guiding and remote launch control, characterized in that the launch device comprises: a fuse against spontaneous launch of the rocket, hinged grips, a wedge-shaped slider forms for holding the rocket and a tension spring for removing grips at startup, an air pipe with a nipple for supplying compressed air to the motor housing, and on the housing of the starting device al for fixing the screw to the guide console. 2. Комплекс по п.1, отличающийся тем, что ракета выполнена из трех блоков - головного обтекателя с амортизатором, корпуса-двигателя с навинчивающимся соплом и блока стабилизаторов.2. The complex according to claim 1, characterized in that the rocket is made of three blocks - a head fairing with a shock absorber, a motor housing with a screw nozzle and a block of stabilizers. 3. Комплекс по п.1, отличающийся тем, что сопло выполнено на резьбе, что позволяет быстро менять сопла с различными диаметрами выходного отверстия, регулируя этим дальность и скорость полета.3. The complex according to claim 1, characterized in that the nozzle is made on a thread, which allows you to quickly change the nozzle with different diameters of the outlet, thereby controlling the range and speed of flight. 4. Комплекс по п.1, отличающийся тем, что модельную ракету изготавливают из пластиковых емкостей из-под напитков.4. The complex according to claim 1, characterized in that the model rocket is made of plastic containers for drinks. 5. Комплекс по п.1, отличающийся тем, что он содержит направляющую консоль достаточной длины с тягой, электромотором-редуктором, проводами и источником питания для дистанционного управления пуском ракеты.5. The complex according to claim 1, characterized in that it contains a guide console of sufficient length with traction, an electric motor-reducer, wires and a power source for remote control of rocket launch. 6. Комплекс по п.1, отличающийся тем, что он выполнен разборным, а опоры основания складывающимися.6. The complex according to claim 1, characterized in that it is made collapsible, and the base supports are folding.
RU2006132135/12A 2006-09-06 2006-09-06 Model of missile complex RU2328330C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2006132135/12A RU2328330C1 (en) 2006-09-06 2006-09-06 Model of missile complex

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2006132135/12A RU2328330C1 (en) 2006-09-06 2006-09-06 Model of missile complex

Publications (2)

Publication Number Publication Date
RU2006132135A true RU2006132135A (en) 2008-03-20
RU2328330C1 RU2328330C1 (en) 2008-07-10

Family

ID=39279336

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2006132135/12A RU2328330C1 (en) 2006-09-06 2006-09-06 Model of missile complex

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RU (1) RU2328330C1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106887181A (en) * 2017-02-25 2017-06-23 佛山市三水区希望火炬教育科技有限公司 A kind of special ship to air missile model of teenager's research in defense-related science and technology

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2503912C1 (en) * 2012-05-04 2014-01-10 Открытое акционерное общество "Завод им. В.А. Дегтярева" Training set for operators of portable air defence missile systems
CN108639369A (en) * 2018-04-27 2018-10-12 宋忠春 A kind of model plane JATO engine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106887181A (en) * 2017-02-25 2017-06-23 佛山市三水区希望火炬教育科技有限公司 A kind of special ship to air missile model of teenager's research in defense-related science and technology

Also Published As

Publication number Publication date
RU2328330C1 (en) 2008-07-10

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MM4A The patent is invalid due to non-payment of fees

Effective date: 20090907