RU2482029C2 - Rocket - Google Patents
Rocket Download PDFInfo
- Publication number
- RU2482029C2 RU2482029C2 RU2011128472/11A RU2011128472A RU2482029C2 RU 2482029 C2 RU2482029 C2 RU 2482029C2 RU 2011128472/11 A RU2011128472/11 A RU 2011128472/11A RU 2011128472 A RU2011128472 A RU 2011128472A RU 2482029 C2 RU2482029 C2 RU 2482029C2
- Authority
- RU
- Russia
- Prior art keywords
- plates
- rocket
- rectangular
- cone
- degrees
- Prior art date
Links
Images
Landscapes
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Braking Arrangements (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 расширение диапазона ракеты.The technical result is the expansion of the range of the rocket.
Технический результат достигается тем, что ракета имеет корпус, состоящий из конуса с прямоугольными пластинами, сверху которых находятся откидные прямоугольные пластины.The technical result is achieved in that the rocket has a housing consisting of a cone with rectangular plates, on top of which are folding rectangular plates.
На фиг.1 показана ракета, на фиг.2 - вид А сверху.In Fig.1 shows a rocket, in Fig.2 is a top view And.
Конструкция включает конус 1, к которому присоединены прямоугольные пластины 2. К корпусу 1 присоединены втулки 3, в которые вставлены оси 4. К осям 4 прикреплены откидные прямоугольные пластины 5.The design includes a cone 1 to which rectangular plates 2 are attached. Sleeve 3 is attached to the housing 1, into which axles 4 are inserted. Hinged rectangular plates 5 are attached to the axles 4.
Оси 4 приводятся в движение от мотор-редуктора 6.Axes 4 are driven by a gear motor 6.
Конструкция работает следующим образом.The design works as follows.
Для плавного приземления ракеты нужно включить мотор-редуктор 6, тогда откидные прямоугольные пластины 5, прикрепленные к осям 4, повернутся на 180 градусов и ракета 6 плавно приземлится.For smooth rocket landing, you need to turn on the gear motor 6, then the folding rectangular plates 5 attached to the axes 4 will rotate 180 degrees and the rocket 6 will land smoothly.
Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2011128472/11A RU2482029C2 (en) | 2011-07-08 | 2011-07-08 | Rocket |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2011128472/11A RU2482029C2 (en) | 2011-07-08 | 2011-07-08 | Rocket |
Publications (2)
Publication Number | Publication Date |
---|---|
RU2011128472A RU2011128472A (en) | 2012-02-20 |
RU2482029C2 true RU2482029C2 (en) | 2013-05-20 |
Family
ID=45854325
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU2011128472/11A RU2482029C2 (en) | 2011-07-08 | 2011-07-08 | Rocket |
Country Status (1)
Country | Link |
---|---|
RU (1) | RU2482029C2 (en) |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2960291A (en) * | 1957-08-16 | 1960-11-15 | Richard F Patterson | Articulated arm aerodynamic drag device |
US3048357A (en) * | 1961-03-23 | 1962-08-07 | Alfred C Loedding | Winglet drogue for aerial refueling |
RU2090445C1 (en) * | 1994-04-19 | 1997-09-20 | Сергей Владимирович Овсянников | Aircraft aerodynamic configuration |
-
2011
- 2011-07-08 RU RU2011128472/11A patent/RU2482029C2/en active
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2960291A (en) * | 1957-08-16 | 1960-11-15 | Richard F Patterson | Articulated arm aerodynamic drag device |
US3048357A (en) * | 1961-03-23 | 1962-08-07 | Alfred C Loedding | Winglet drogue for aerial refueling |
RU2090445C1 (en) * | 1994-04-19 | 1997-09-20 | Сергей Владимирович Овсянников | Aircraft aerodynamic configuration |
Also Published As
Publication number | Publication date |
---|---|
RU2011128472A (en) | 2012-02-20 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
MX2014012371A (en) | Thrust absorbing planetary traction drive superturbo. | |
RU2017110703A (en) | MULTICOPTER WITH A SWIVEL WING | |
WO2015134170A3 (en) | Powered landing gear | |
GB2533982A (en) | Drive system for aircraft landing gear | |
RU2482029C2 (en) | Rocket | |
EP3487723A4 (en) | Power take-off drive gear thrust load canceling | |
BR112016013784A2 (en) | PLANETARY GEAR, WIND GENERATOR COMPRISING A PLANETARY GEAR AND USE OF A PLANETARY GEAR | |
WO2013131201A3 (en) | Combustion engine | |
RU2444467C2 (en) | Rocket | |
RU2444468C2 (en) | Rocket | |
RU2449929C2 (en) | Spacecraft | |
WO2012098021A3 (en) | Rudder propeller | |
RU2419061C2 (en) | Missile | |
RU2407664C2 (en) | Rocket | |
RU2016128032A (en) | MODULE WITH ARTIFICIAL GRAVITY FOR RESIDENCE OF COSMONAUTS ON INTERPLANETARY FLIGHTS | |
RU2443608C2 (en) | Rocket | |
RU2007102769A (en) | METHOD FOR MOVING AN OBJECT IN SPACE | |
RU2458829C2 (en) | Spacecraft | |
Brownlee | Comets | |
Janssen | Deep Atmospheres of Saturn and Jupiter Observed from Orbiting Spacecraft | |
RU2449921C2 (en) | Spacecraft | |
RU2014123606A (en) | SIDE AIRPLANE CONTROL KNOB | |
RU2534159C2 (en) | Control method for aircraft (ac) of helicopter type | |
Sheppard et al. | Comet 324P/2015 K3 (la Sagra) | |
Jewitt | Hubble imaging of a newly discovered active asteroid |