RU2443601C2 - Rocket - Google Patents

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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
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RU
Russia
Prior art keywords
disk
rocket
hyperboloid
nozzles
cable
Prior art date
Application number
RU2010143927/11A
Other languages
Russian (ru)
Other versions
RU2010143927A (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.)
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Publication date
Application filed by Александр Михайлович Гультяев filed Critical Александр Михайлович Гультяев
Priority to RU2010143927/11A priority Critical patent/RU2443601C2/en
Publication of RU2010143927A publication Critical patent/RU2010143927A/en
Application granted granted Critical
Publication of RU2443601C2 publication Critical patent/RU2443601C2/en

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  • Manufacture, Treatment Of Glass Fibers (AREA)
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Abstract

FIELD: transport.
SUBSTANCE: invention relates to aerospace engineering. Proposed rocket comprises disk with deflecting nozzles and cable to be reeled on one-way hyperboloid fitted on said disk.
EFFECT: expanded operating performances.
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 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)

Ракета, отличающаяся тем, что содержит диск с отклоняющими соплами, и трос, выполненный с возможностью наматывания на закрепленный на диске однополосный гиперболоид. A missile, characterized in that it contains a disk with deflecting nozzles, and a cable made with the possibility of winding on a single-band hyperboloid mounted on the disk.
RU2010143927/11A 2010-10-26 2010-10-26 Rocket RU2443601C2 (en)

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)

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RU (1) RU2443601C2 (en)

Citations (4)

* Cited by examiner, † Cited by third party
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

Patent Citations (4)

* Cited by examiner, † Cited by third party
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

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Publication number Publication date
RU2010143927A (en) 2011-02-20

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