RU2375268C2 - Rocket - Google Patents
Rocket Download PDFInfo
- Publication number
- RU2375268C2 RU2375268C2 RU2008134408/11A RU2008134408A RU2375268C2 RU 2375268 C2 RU2375268 C2 RU 2375268C2 RU 2008134408/11 A RU2008134408/11 A RU 2008134408/11A RU 2008134408 A RU2008134408 A RU 2008134408A RU 2375268 C2 RU2375268 C2 RU 2375268C2
- Authority
- RU
- Russia
- Prior art keywords
- rocket
- stabilizer
- movable blades
- housing
- hinged wings
- Prior art date
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- Inorganic Compounds Of Heavy Metals (AREA)
- Vehicle Body Suspensions (AREA)
- Hinges (AREA)
Abstract
Description
Изобретение относится к космонавтике и служит для полета в космосе.The invention relates to astronautics and is used for flight in space.
Известна конструкция ракеты (см. «Политехнический словарь». И.И. Артоболевский. Советская энциклопедия. М., 1977, стр.412), состоящей из корпуса и стабилизатора.The design of the rocket is known (see. "Polytechnical Dictionary". II Artobolevsky. Soviet Encyclopedia. M., 1977, p. 412), consisting of a body and a stabilizer.
Данная ракета не планирует.This rocket does not plan.
Изобретение направлено на устранение указанного недостатка.The invention is aimed at eliminating this drawback.
Достигается тем, что стабилизатор имеет в верхней части две подвижные лопасти в виде откидных крыльев.This is achieved by the fact that the stabilizer has in the upper part two movable blades in the form of hinged wings.
На фиг.1 показана ракета, на фиг.2 - ее вид сбоку. На фиг.3 - ракета при планировании, на фиг.4 - вид сбоку при ее планировании.Figure 1 shows a rocket, figure 2 is a side view of it. Figure 3 - rocket when planning, figure 4 is a side view when planning it.
Конструкция включает корпус 1, к которому крепится стабилизатор 2. К стабилизатору 2 подвижно крепятся подвижные лопасти 3.The design includes a housing 1 to which the stabilizer 2 is attached. Mobile blades 3 are movably mounted to the stabilizer 2.
Устройство работает следующим образом.The device operates as follows.
При снижении ракеты подвижные лопасти 3 раскладываются в разные стороны и ракета планирует.With the decrease of the rocket, the movable blades 3 are laid out in different directions and the rocket plans.
Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2008134408/11A RU2375268C2 (en) | 2008-08-21 | 2008-08-21 | Rocket |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2008134408/11A RU2375268C2 (en) | 2008-08-21 | 2008-08-21 | Rocket |
Publications (2)
Publication Number | Publication Date |
---|---|
RU2008134408A RU2008134408A (en) | 2008-12-27 |
RU2375268C2 true RU2375268C2 (en) | 2009-12-10 |
Family
ID=41489780
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU2008134408/11A RU2375268C2 (en) | 2008-08-21 | 2008-08-21 | Rocket |
Country Status (1)
Country | Link |
---|---|
RU (1) | RU2375268C2 (en) |
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2008
- 2008-08-21 RU RU2008134408/11A patent/RU2375268C2/en active
Also Published As
Publication number | Publication date |
---|---|
RU2008134408A (en) | 2008-12-27 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
TK4A | Correction to the publication in the bulletin (patent) |
Free format text: AMENDMENT TO CHAPTER -FG4A- IN JOURNAL: 34-2009 |