RU2444467C2 - Rocket - Google Patents

Rocket Download PDF

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Publication number
RU2444467C2
RU2444467C2 RU2010148925/11A RU2010148925A RU2444467C2 RU 2444467 C2 RU2444467 C2 RU 2444467C2 RU 2010148925/11 A RU2010148925/11 A RU 2010148925/11A RU 2010148925 A RU2010148925 A RU 2010148925A RU 2444467 C2 RU2444467 C2 RU 2444467C2
Authority
RU
Russia
Prior art keywords
cones
rocket
movable
space
shafts
Prior art date
Application number
RU2010148925/11A
Other languages
Russian (ru)
Other versions
RU2010148925A (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 RU2010148925/11A priority Critical patent/RU2444467C2/en
Publication of RU2010148925A publication Critical patent/RU2010148925A/en
Application granted granted Critical
Publication of RU2444467C2 publication Critical patent/RU2444467C2/en

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

Abstract

FIELD: transport.
SUBSTANCE: invention relates to space engineering and is intended for space flights. Rocket consists of body 1 equipped with movable cones 2 fitted one into another at body top section. Said movable cones 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.

Это достигается тем, что ракета имеет четыре пустотелых подвижных конуса, которые находятся один в другом.This is achieved by the fact that the rocket has four hollow movable cones, which are one in the other.

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 конуса 2. Подвижные конуса 2 крепятся к валам 3 моторедуктора 4.The design includes a housing 1, in the upper part of which there are movable cones 2. The movable cones 2 are attached to the shafts 3 of the gear motor 4.

Конструкция работает следующим образом: для плавного приземления ракеты нужно включить моторедуктор 4, который развернет по очереди подвижные конуса 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 gearmotor 4, which will rotate the moving cones 2 180 degrees in turn, and the rocket will land smoothly.

Claims (1)

Ракета, отличающаяся тем, что имеет четыре пустотелых подвижных конуса, имеющих возможность разворота на 180°, крепящихся к валам моторедуктора, при этом конусы находятся один в другом. A missile, characterized in that it has four hollow movable cones having a 180 ° turn possibility, attached to the shafts of the gearmotor, while the cones are one in the other.
RU2010148925/11A 2010-11-30 2010-11-30 Rocket RU2444467C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2010148925/11A RU2444467C2 (en) 2010-11-30 2010-11-30 Rocket

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2010148925/11A RU2444467C2 (en) 2010-11-30 2010-11-30 Rocket

Publications (2)

Publication Number Publication Date
RU2010148925A RU2010148925A (en) 2011-03-10
RU2444467C2 true RU2444467C2 (en) 2012-03-10

Family

ID=46029197

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2010148925/11A RU2444467C2 (en) 2010-11-30 2010-11-30 Rocket

Country Status (1)

Country Link
RU (1) RU2444467C2 (en)

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
RU2328410C1 (en) * 2007-02-20 2008-07-10 Федеральное государственное унитарное предприятие "Центральный научно-исследовательский институт машиностроения" (ФГУП ЦНИИмаш) Fairing of rocket launcher

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
RU2328410C1 (en) * 2007-02-20 2008-07-10 Федеральное государственное унитарное предприятие "Центральный научно-исследовательский институт машиностроения" (ФГУП ЦНИИмаш) Fairing of rocket launcher
RU67463U1 (en) * 2007-06-01 2007-10-27 Общество С Ограниченной Ответственностью "Трибека" TOY BUILDING SET

Also Published As

Publication number Publication date
RU2010148925A (en) 2011-03-10

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