RU2444468C2 - Rocket - Google Patents
Rocket Download PDFInfo
- 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
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Abstract
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
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
Claims (1)
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)
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 |
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2010
- 2010-11-30 RU RU2010148926/11A patent/RU2444468C2/en active
Patent Citations (3)
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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