RU2008125390A - HYBRID ROCKET - Google Patents
HYBRID ROCKET Download PDFInfo
- Publication number
- RU2008125390A RU2008125390A RU2008125390/02A RU2008125390A RU2008125390A RU 2008125390 A RU2008125390 A RU 2008125390A RU 2008125390/02 A RU2008125390/02 A RU 2008125390/02A RU 2008125390 A RU2008125390 A RU 2008125390A RU 2008125390 A RU2008125390 A RU 2008125390A
- Authority
- RU
- Russia
- Prior art keywords
- rocket
- head
- missile
- engine
- hybrid
- Prior art date
Links
Landscapes
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
1. Гибридная ракета, включающая отделяющуюся хвостовую часть и головную часть, причем головная часть представляет собой крылатую ракету, снабженную собственным двигателем для самостоятельного движения к цели. ! 2. Гибридная ракета по п.1, включающая отделяющуюся хвостовую часть и головную часть, причем ракета снабжена устройством "антикрыло перед соплом", включающим ракетный двигатель, сопло которого направлено против движения ракеты, и расположенное в газовом потоке упомянутого ракетного двигателя антикрыло с управляемым углом атаки для тормозящего снижения ракеты.1. A hybrid missile, including a detachable tail and a head, and the head is a cruise missile equipped with its own engine for independent movement to the target. ! 2. The hybrid rocket according to claim 1, comprising a detachable tail section and a head section, wherein the rocket is equipped with a “wing in front of the nozzle” device, comprising a rocket engine, the nozzle of which is directed against the movement of the rocket, and a wing with a controlled angle located in the gas stream of said rocket engine attacks for braking missile descent.
Claims (2)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2008125390/02A RU2383851C1 (en) | 2008-06-20 | 2008-06-20 | Hydrid rocket |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2008125390/02A RU2383851C1 (en) | 2008-06-20 | 2008-06-20 | Hydrid rocket |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| RU2008125390A true RU2008125390A (en) | 2009-12-27 |
| RU2383851C1 RU2383851C1 (en) | 2010-03-10 |
Family
ID=41642546
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| RU2008125390/02A RU2383851C1 (en) | 2008-06-20 | 2008-06-20 | Hydrid rocket |
Country Status (1)
| Country | Link |
|---|---|
| RU (1) | RU2383851C1 (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2739537C1 (en) * | 2020-06-25 | 2020-12-25 | Федеральное казенное предприятие "Научно-исследовательский институт "Геодезия" (ФКП "НИИ "Геодезия") | Rocket carriage with controlled braking |
-
2008
- 2008-06-20 RU RU2008125390/02A patent/RU2383851C1/en active
Also Published As
| Publication number | Publication date |
|---|---|
| RU2383851C1 (en) | 2010-03-10 |
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