RU2375670C2 - Rocket - Google Patents

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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
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RU
Russia
Prior art keywords
rocket
landing
engineering
stabilizer
airspace
Prior art date
Application number
RU2008130170/11A
Other languages
Russian (ru)
Other versions
RU2008130170A (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 RU2008130170/11A priority Critical patent/RU2375670C2/en
Publication of RU2008130170A publication Critical patent/RU2008130170A/en
Application granted granted Critical
Publication of RU2375670C2 publication Critical patent/RU2375670C2/en

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  • Vehicle Body Suspensions (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

FIELD: aerospace engineering.
SUBSTANCE: invention relates to airspace engineering and can be used for smooth landing of rocket. Proposed rocket consists of engine housing and control surfaces representing an elastically-deformable cylindrical tape with detachable end.
EFFECT: rocket gliding in landing.
3 dwg

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 detachable mounting end 4.

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 engine 2. Cylindrical stabilizers 3 with one removable-fixing end 4 are attached to the housing 1. The design works as follows.

При опускании ракеты вниз съемно-крепежный конец 4 отцепляется, цилиндрические стабилизаторы 3 выпрямляются и ракета планирует вниз.When lowering the rocket down, the removable mounting end 4 is detached, the cylindrical stabilizers 3 are straightened and the rocket is planning down.

Claims (1)

Ракета, состоящая из корпуса двигателя и стабилизатора, отличающаяся тем, что стабилизатор выполнен в виде упругой деформирующей ленты в форме цилиндра со съемно-крепленным концом. A rocket consisting of a motor housing and a stabilizer, characterized in that the stabilizer is made in the form of an elastic deforming tape in the form of a cylinder with a removable fastened end.
RU2008130170/11A 2008-07-21 2008-07-21 Rocket RU2375670C2 (en)

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)

Also Published As

Publication number Publication date
RU2008130170A (en) 2008-12-27

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