RU2443600C2 - Rocket - Google Patents
Rocket Download PDFInfo
- Publication number
- RU2443600C2 RU2443600C2 RU2010148373/11A RU2010148373A RU2443600C2 RU 2443600 C2 RU2443600 C2 RU 2443600C2 RU 2010148373/11 A RU2010148373/11 A RU 2010148373/11A RU 2010148373 A RU2010148373 A RU 2010148373A RU 2443600 C2 RU2443600 C2 RU 2443600C2
- Authority
- RU
- Russia
- Prior art keywords
- bottom sections
- rocket
- additionally
- engine
- transport
- Prior art date
Links
Images
Landscapes
- Transmission Devices (AREA)
- Hinges (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
Description
Изобретение относится к космонавтике и служит для транспортировки приборов в космосе.The invention relates to astronautics and is used to transport instruments in space.
Техническим результатом является увеличение диапазона ракеты.The technical result is to increase the range of the rocket.
Достигается тем, что имеет корпус с подвижно-шарнирными пластинами.This is achieved by the fact that it has a housing with movable-hinged plates.
На фиг.1 показана ракета, на фиг.2 - вид А снизу. Figure 1 shows the rocket, figure 2 is a view A from below.
Конструкция состоит из верхней части 1 и нижней части 2, которые соединены подвижно-шарнирными пластинами 3. Подвижно-шарнирные пластины 3 соединены шарнирами 4. Верхняя часть 1 и нижняя часть соединены винтом 5, который приводится во вращение двигателем 6. Конструкция работает следующим образом: для плавного приземления ракеты нужно включить электродвигатель 6, который приведет во вращение винт 5, тогда верхняя часть 1 станет сближаться с нижней частью 2, а подвижно-шарнирные пластины 3 образуют юбку, что дает плавное приземления ракеты.The design consists of the upper part 1 and the lower part 2, which are connected by movable-hinge plates 3. The movable-hinge plates 3 are connected by hinges 4. The upper part 1 and the lower part are connected by a screw 5, which is driven by the engine 6. The design works as follows: for a smooth landing of the rocket, you need to turn on the electric motor 6, which will rotate the screw 5, then the upper part 1 will come closer to the lower part 2, and the movable-hinged plates 3 form a skirt, which gives a smooth landing of the rocket.
Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2010148373/11A RU2443600C2 (en) | 2010-11-26 | 2010-11-26 | Rocket |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2010148373/11A RU2443600C2 (en) | 2010-11-26 | 2010-11-26 | Rocket |
Publications (2)
Publication Number | Publication Date |
---|---|
RU2010148373A RU2010148373A (en) | 2011-03-10 |
RU2443600C2 true RU2443600C2 (en) | 2012-02-27 |
Family
ID=45852462
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU2010148373/11A RU2443600C2 (en) | 2010-11-26 | 2010-11-26 | Rocket |
Country Status (1)
Country | Link |
---|---|
RU (1) | RU2443600C2 (en) |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB208493A (en) * | 1923-08-13 | 1923-12-20 | Hans Peter Hansen | Improvements in signal rockets |
RU199U1 (en) * | 1993-08-10 | 1995-01-16 | Машиностроительное Конструкторское Бюро "Факел" | Wing opening mechanism |
RU2075722C1 (en) * | 1993-11-30 | 1997-03-20 | Юлий Борисович Лакоткин | Process of filling of model of rocket with working medium and structure for its implementation |
RU2234442C2 (en) * | 2002-08-05 | 2004-08-20 | Федеральное государственное унитарное предприятие Государственный ракетный центр "КБ им. акад. В.П. Макеева" | Descent spacecraft |
-
2010
- 2010-11-26 RU RU2010148373/11A patent/RU2443600C2/en active
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB208493A (en) * | 1923-08-13 | 1923-12-20 | Hans Peter Hansen | Improvements in signal rockets |
RU199U1 (en) * | 1993-08-10 | 1995-01-16 | Машиностроительное Конструкторское Бюро "Факел" | Wing opening mechanism |
RU2075722C1 (en) * | 1993-11-30 | 1997-03-20 | Юлий Борисович Лакоткин | Process of filling of model of rocket with working medium and structure for its implementation |
RU2234442C2 (en) * | 2002-08-05 | 2004-08-20 | Федеральное государственное унитарное предприятие Государственный ракетный центр "КБ им. акад. В.П. Макеева" | Descent spacecraft |
Also Published As
Publication number | Publication date |
---|---|
RU2010148373A (en) | 2011-03-10 |
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