RU2443601C2 - Rocket - Google Patents
Rocket Download PDFInfo
- Publication number
- RU2443601C2 RU2443601C2 RU2010143927/11A RU2010143927A RU2443601C2 RU 2443601 C2 RU2443601 C2 RU 2443601C2 RU 2010143927/11 A RU2010143927/11 A RU 2010143927/11A RU 2010143927 A RU2010143927 A RU 2010143927A RU 2443601 C2 RU2443601 C2 RU 2443601C2
- Authority
- RU
- Russia
- Prior art keywords
- disk
- rocket
- hyperboloid
- nozzles
- cable
- Prior art date
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- Toys (AREA)
- Manufacture, Treatment Of Glass Fibers (AREA)
- Tires In General (AREA)
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 однополосный гиперболоид и диск с отклоняющимися соплами, отклоняющиеся сопла расположены на концах диска.This is achieved by having a single-lane hyperboloid and a disk with deviating nozzles, deviating nozzles are located at the ends of the disk.
На фиг.1 показана ракета, на фиг.2 вид - А снизу.Figure 1 shows a rocket, figure 2 view - And from the bottom.
Конструкция включает: диск 1, на котором находятся отклоняющиеся сопла 2. К диску 1 крепится однополосный гиперболоид 3, на котором намотан гибкий трос 4.The design includes: a disk 1, on which there are deviating nozzles 2. A single-band hyperboloid 3 is attached to the disk 1, on which a flexible cable 4 is wound.
Конструкция работает следующим образом. Для намотки гибкого троса 4, который прикреплен к летящему астероиду, нужно отклонить отклоняющиеся сопла 2 на 90 градусов так, чтобы они работали по касательной к диску 1. Таким образом ракета будет вращаться, а в гибкий трос 4 - наматываться.The design works as follows. To wind a flexible cable 4, which is attached to a flying asteroid, you need to deflect the deviating nozzles 2 90 degrees so that they work tangentially to the disk 1. Thus, the rocket will rotate, and the flexible cable 4 will be wound.
Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2010143927/11A RU2443601C2 (en) | 2010-10-26 | 2010-10-26 | Rocket |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2010143927/11A RU2443601C2 (en) | 2010-10-26 | 2010-10-26 | Rocket |
Publications (2)
Publication Number | Publication Date |
---|---|
RU2010143927A RU2010143927A (en) | 2011-02-20 |
RU2443601C2 true RU2443601C2 (en) | 2012-02-27 |
Family
ID=45852464
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU2010143927/11A RU2443601C2 (en) | 2010-10-26 | 2010-10-26 | Rocket |
Country Status (1)
Country | Link |
---|---|
RU (1) | RU2443601C2 (en) |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0807578A1 (en) * | 1996-05-17 | 1997-11-19 | Matra Marconi Space France S.A. | Controlling rotation of a spacecraft |
RU2002133269A (en) * | 2002-12-11 | 2004-06-20 | Олег Александрович Александров | METHOD OF REUSABLE LAYING AND DEPLOYMENT IN SPACE OF EXTRA FRAMELESS FRAMELESS DESIGNS OF FLAT OR CONVEX-CONCAVED FORMS, AND SAILING-REFLECTOR SPACE APPAREGEROGO |
RU2309876C1 (en) * | 2006-05-23 | 2007-11-10 | Федеральное государственное научное учреждение "Государственный научно-исследовательский институт прикладной механики и электродинамики" (ФГНУ "НИИ ПМЭ") | Method of control of spacecraft motion and control system for realization of this method |
CN101746505A (en) * | 2010-02-10 | 2010-06-23 | 哈尔滨盛世特种飞行器有限公司 | Disc-shaped unmanned aircraft of single-thrust paddle |
-
2010
- 2010-10-26 RU RU2010143927/11A patent/RU2443601C2/en active
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0807578A1 (en) * | 1996-05-17 | 1997-11-19 | Matra Marconi Space France S.A. | Controlling rotation of a spacecraft |
RU2002133269A (en) * | 2002-12-11 | 2004-06-20 | Олег Александрович Александров | METHOD OF REUSABLE LAYING AND DEPLOYMENT IN SPACE OF EXTRA FRAMELESS FRAMELESS DESIGNS OF FLAT OR CONVEX-CONCAVED FORMS, AND SAILING-REFLECTOR SPACE APPAREGEROGO |
RU2309876C1 (en) * | 2006-05-23 | 2007-11-10 | Федеральное государственное научное учреждение "Государственный научно-исследовательский институт прикладной механики и электродинамики" (ФГНУ "НИИ ПМЭ") | Method of control of spacecraft motion and control system for realization of this method |
CN101746505A (en) * | 2010-02-10 | 2010-06-23 | 哈尔滨盛世特种飞行器有限公司 | Disc-shaped unmanned aircraft of single-thrust paddle |
Also Published As
Publication number | Publication date |
---|---|
RU2010143927A (en) | 2011-02-20 |
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