RU2482029C2 - Rocket - Google Patents

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Publication number
RU2482029C2
RU2482029C2 RU2011128472/11A RU2011128472A RU2482029C2 RU 2482029 C2 RU2482029 C2 RU 2482029C2 RU 2011128472/11 A RU2011128472/11 A RU 2011128472/11A RU 2011128472 A RU2011128472 A RU 2011128472A RU 2482029 C2 RU2482029 C2 RU 2482029C2
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RU
Russia
Prior art keywords
plates
rocket
rectangular
cone
degrees
Prior art date
Application number
RU2011128472/11A
Other languages
Russian (ru)
Other versions
RU2011128472A (en
Inventor
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 RU2011128472/11A priority Critical patent/RU2482029C2/en
Publication of RU2011128472A publication Critical patent/RU2011128472A/en
Application granted granted Critical
Publication of RU2482029C2 publication Critical patent/RU2482029C2/en

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Abstract

FIELD: transport.
SUBSTANCE: invention relates to aerospace engineering, particularly, to space rocket. Proposed rocket comprises body shaped to cone with rectangular plates. Rectangular hinged plates are arranged above aforesaid plates to turn through 180 degrees on shafts driven by geared motor.
EFFECT: smooth landing.
2 dwg

Description

Изобретение относится к космонавтике и служит для полетов астронавтов в космосе.The invention relates to astronautics and is used for astronaut flights in space.

Техническим результатом является расширение диапазона ракеты.The technical result is the expansion of the range of the rocket.

Технический результат достигается тем, что ракета имеет корпус, состоящий из конуса с прямоугольными пластинами, сверху которых находятся откидные прямоугольные пластины.The technical result is achieved in that the rocket has a housing consisting of a cone with rectangular plates, on top of which are folding rectangular plates.

На фиг.1 показана ракета, на фиг.2 - вид А сверху.In Fig.1 shows a rocket, in Fig.2 is a top view And.

Конструкция включает конус 1, к которому присоединены прямоугольные пластины 2. К корпусу 1 присоединены втулки 3, в которые вставлены оси 4. К осям 4 прикреплены откидные прямоугольные пластины 5.The design includes a cone 1 to which rectangular plates 2 are attached. Sleeve 3 is attached to the housing 1, into which axles 4 are inserted. Hinged rectangular plates 5 are attached to the axles 4.

Оси 4 приводятся в движение от мотор-редуктора 6.Axes 4 are driven by a gear motor 6.

Конструкция работает следующим образом.The design works as follows.

Для плавного приземления ракеты нужно включить мотор-редуктор 6, тогда откидные прямоугольные пластины 5, прикрепленные к осям 4, повернутся на 180 градусов и ракета 6 плавно приземлится.For smooth rocket landing, you need to turn on the gear motor 6, then the folding rectangular plates 5 attached to the axes 4 will rotate 180 degrees and the rocket 6 will land smoothly.

Claims (1)

Ракета, отличающаяся тем, что имеет корпус, выполненный в виде конуса с прямоугольными пластинами, сверху которых установлены прямоугольные откидные пластины, выполненные с возможностью поворота на 180° на осях, приводимых в движение моторедуктором. A missile, characterized in that it has a housing made in the form of a cone with rectangular plates, on top of which are mounted rectangular folding plates, made with the possibility of rotation through 180 ° on the axes, driven by a gear motor.
RU2011128472/11A 2011-07-08 2011-07-08 Rocket RU2482029C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2011128472/11A RU2482029C2 (en) 2011-07-08 2011-07-08 Rocket

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2011128472/11A RU2482029C2 (en) 2011-07-08 2011-07-08 Rocket

Publications (2)

Publication Number Publication Date
RU2011128472A RU2011128472A (en) 2012-02-20
RU2482029C2 true RU2482029C2 (en) 2013-05-20

Family

ID=45854325

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2011128472/11A RU2482029C2 (en) 2011-07-08 2011-07-08 Rocket

Country Status (1)

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RU (1) RU2482029C2 (en)

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2960291A (en) * 1957-08-16 1960-11-15 Richard F Patterson Articulated arm aerodynamic drag device
US3048357A (en) * 1961-03-23 1962-08-07 Alfred C Loedding Winglet drogue for aerial refueling
RU2090445C1 (en) * 1994-04-19 1997-09-20 Сергей Владимирович Овсянников Aircraft aerodynamic configuration

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2960291A (en) * 1957-08-16 1960-11-15 Richard F Patterson Articulated arm aerodynamic drag device
US3048357A (en) * 1961-03-23 1962-08-07 Alfred C Loedding Winglet drogue for aerial refueling
RU2090445C1 (en) * 1994-04-19 1997-09-20 Сергей Владимирович Овсянников Aircraft aerodynamic configuration

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Publication number Publication date
RU2011128472A (en) 2012-02-20

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