RU2444468C2 - Rocket - Google Patents

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Publication number
RU2444468C2
RU2444468C2 RU2010148926/11A RU2010148926A RU2444468C2 RU 2444468 C2 RU2444468 C2 RU 2444468C2 RU 2010148926/11 A RU2010148926/11 A RU 2010148926/11A RU 2010148926 A RU2010148926 A RU 2010148926A RU 2444468 C2 RU2444468 C2 RU 2444468C2
Authority
RU
Russia
Prior art keywords
rocket
spheres
movable semi
space
shafts
Prior art date
Application number
RU2010148926/11A
Other languages
Russian (ru)
Other versions
RU2010148926A (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 RU2010148926/11A priority Critical patent/RU2444468C2/en
Publication of RU2010148926A publication Critical patent/RU2010148926A/en
Application granted granted Critical
Publication of RU2444468C2 publication Critical patent/RU2444468C2/en

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Abstract

FIELD: transport.
SUBSTANCE: invention relates to space engineering and is intended for space flights. Rocket consists of body 1 equipped with movable semi-spheres 2 fitted one into another at body top section. Said movable semi-spheres are attached to shafts 3 of geared motor 4 to turn said cones through 180°.
EFFECT: higher reliability.
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 увеличение диапазона ракеты.The technical result is to increase the range of the rocket.

Достигается тем, что имеет четыре пустотелых подвижных полусферы, которые находятся одна в другой.This is achieved by the fact that it has four hollow moving hemispheres, which are located in one another.

На фиг.1 показана ракета, на фиг.2 - разрез А-А.Figure 1 shows a rocket, figure 2 is a section aa.

Конструкция включает корпус 1, в верхней части которого находятся подвижные полусферы 2. Подвижные полусферы 2 крепятся к валам 3 мотор-редукторов 4.The design includes a housing 1, in the upper part of which there are movable hemispheres 2. The movable hemispheres 2 are attached to the shafts 3 of the gear motors 4.

Конструкция работает следующим образом: для плавного приземления ракеты нужно включить мотор-редуктор 4, которые повернут по очереди подвижные полусферы 2 на 180 градусов, и ракета плавно приземлится.The design works as follows: for a smooth landing of the rocket, you need to turn on the gear motor 4, which will rotate the moving hemispheres 2 180 degrees, and the rocket will land smoothly.

Claims (1)

Ракета, отличающаяся тем, что имеет четыре пустотелых подвижных полусферы, имеющие возможность разворота на 180°, крепящиеся к валам мотор-редуктора, при этом полусферы находятся одна в другой. A missile, characterized in that it has four hollow movable hemispheres, with the possibility of a 180 ° turn, attached to the shafts of the geared motor, with the hemispheres being one in the other.
RU2010148926/11A 2010-11-30 2010-11-30 Rocket RU2444468C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2010148926/11A RU2444468C2 (en) 2010-11-30 2010-11-30 Rocket

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2010148926/11A RU2444468C2 (en) 2010-11-30 2010-11-30 Rocket

Publications (2)

Publication Number Publication Date
RU2010148926A RU2010148926A (en) 2011-03-10
RU2444468C2 true RU2444468C2 (en) 2012-03-10

Family

ID=46029198

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2010148926/11A RU2444468C2 (en) 2010-11-30 2010-11-30 Rocket

Country Status (1)

Country Link
RU (1) RU2444468C2 (en)

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2291818C2 (en) * 2000-01-18 2007-01-20 Контравес Спейс Аг Payload skin
RU67463U1 (en) * 2007-06-01 2007-10-27 Общество С Ограниченной Ответственностью "Трибека" TOY BUILDING SET
FR2902472A1 (en) * 2006-06-14 2007-12-21 Eads Space Transp Sas Soc Par Compact temporary mechanical joining device, e.g. for joining satellite to spacecraft, includes segmented annular device with gripping heads, bolting ring and fixed and movable supports

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2291818C2 (en) * 2000-01-18 2007-01-20 Контравес Спейс Аг Payload skin
FR2902472A1 (en) * 2006-06-14 2007-12-21 Eads Space Transp Sas Soc Par Compact temporary mechanical joining device, e.g. for joining satellite to spacecraft, includes segmented annular device with gripping heads, bolting ring and fixed and movable supports
RU67463U1 (en) * 2007-06-01 2007-10-27 Общество С Ограниченной Ответственностью "Трибека" TOY BUILDING SET

Also Published As

Publication number Publication date
RU2010148926A (en) 2011-03-10

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