RU2375268C2 - Rocket - Google Patents

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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
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RU
Russia
Prior art keywords
rocket
stabilizer
movable blades
housing
hinged wings
Prior art date
Application number
RU2008134408/11A
Other languages
Russian (ru)
Other versions
RU2008134408A (en
Inventor
Александр Михайлович Гультяев (RU)
Александр Михайлович Гультяев
Original Assignee
Александр Михайлович Гультяев
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 Александр Михайлович Гультяев filed Critical Александр Михайлович Гультяев
Priority to RU2008134408/11A priority Critical patent/RU2375268C2/en
Publication of RU2008134408A publication Critical patent/RU2008134408A/en
Application granted granted Critical
Publication of RU2375268C2 publication Critical patent/RU2375268C2/en

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  • Inorganic Compounds Of Heavy Metals (AREA)
  • Vehicle Body Suspensions (AREA)
  • Hinges (AREA)

Abstract

FIELD: aerospace engineering.
SUBSTANCE: proposed rocket consists of housing and control surfaces made up of two movable blades representing hinged wings.
EFFECT: rocket gliding.
4 dwg

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)

Ракета, состоящая из корпуса и стабилизатора, отличающаяся тем, что стабилизатор имеет в верхней части две подвижные лопасти в виде откидных крыльев. A rocket consisting of a body and a stabilizer, characterized in that the stabilizer has two movable blades in the form of hinged wings in the upper part.
RU2008134408/11A 2008-08-21 2008-08-21 Rocket RU2375268C2 (en)

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)

Also Published As

Publication number Publication date
RU2008134408A (en) 2008-12-27

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