RU2375670C2 - Rocket - Google Patents
Rocket Download PDFInfo
- Publication number
- RU2375670C2 RU2375670C2 RU2008130170/11A RU2008130170A RU2375670C2 RU 2375670 C2 RU2375670 C2 RU 2375670C2 RU 2008130170/11 A RU2008130170/11 A RU 2008130170/11A RU 2008130170 A RU2008130170 A RU 2008130170A RU 2375670 C2 RU2375670 C2 RU 2375670C2
- Authority
- RU
- Russia
- Prior art keywords
- rocket
- landing
- engineering
- stabilizer
- airspace
- Prior art date
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- Vehicle Body Suspensions (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
Description
Изобретение относится к космонавтике и служит для плавного приземления ракеты.The invention relates to astronautics and is used for the smooth landing of a rocket.
Известна конструкция ракеты (см. «Политехнический словарь» И.И.Артоболевский. М., 1977 г., стр. 412), состоящей из корпуса, двигателя и стабилизатора.The known design of the rocket (see. "Polytechnical Dictionary" I.I. Artobolevsky. M., 1977, p. 412), consisting of a body, engine and stabilizer.
Данная ракета не планирует при приземлении.This missile does not plan on landing.
Изобретение направлено на устранение данного недостатка.The invention is aimed at eliminating this drawback.
Достигается тем, что стабилизатор выполнен в виде упругой деформирующей ленты в форме цилиндра, с одним съемно-крепежным концом.This is achieved by the fact that the stabilizer is made in the form of an elastic deforming tape in the form of a cylinder, with one removable mounting end.
На фиг.1 изображена ракета, на фиг.2 - вид сбоку и на фиг.3 - вид сверху при отцепившемся съемно-крепежном конце 4.Figure 1 shows a rocket, figure 2 is a side view and figure 3 is a top view of the detached
Ракета состоит из корпуса 1 с двигателем 2. К корпусу 1 крепятся цилиндрические стабилизаторы 3 с одним съемно-крепежным концом 4. Конструкция работает следующим образом.The missile consists of a housing 1 with an
При опускании ракеты вниз съемно-крепежный конец 4 отцепляется, цилиндрические стабилизаторы 3 выпрямляются и ракета планирует вниз.When lowering the rocket down, the
Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2008130170/11A RU2375670C2 (en) | 2008-07-21 | 2008-07-21 | Rocket |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2008130170/11A RU2375670C2 (en) | 2008-07-21 | 2008-07-21 | Rocket |
Publications (2)
Publication Number | Publication Date |
---|---|
RU2008130170A RU2008130170A (en) | 2008-12-27 |
RU2375670C2 true RU2375670C2 (en) | 2009-12-10 |
Family
ID=41489788
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU2008130170/11A RU2375670C2 (en) | 2008-07-21 | 2008-07-21 | Rocket |
Country Status (1)
Country | Link |
---|---|
RU (1) | RU2375670C2 (en) |
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2008
- 2008-07-21 RU RU2008130170/11A patent/RU2375670C2/en active
Also Published As
Publication number | Publication date |
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RU2008130170A (en) | 2008-12-27 |
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