RU2011132614A - SPACE HEAD - Google Patents
SPACE HEAD Download PDFInfo
- Publication number
- RU2011132614A RU2011132614A RU2011132614/11A RU2011132614A RU2011132614A RU 2011132614 A RU2011132614 A RU 2011132614A RU 2011132614/11 A RU2011132614/11 A RU 2011132614/11A RU 2011132614 A RU2011132614 A RU 2011132614A RU 2011132614 A RU2011132614 A RU 2011132614A
- Authority
- RU
- Russia
- Prior art keywords
- joint
- spacecraft
- launch vehicle
- head fairing
- head
- Prior art date
Links
Landscapes
- Moulding By Coating Moulds (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
Космическая головная часть, содержащая космический аппарат и головной обтекатель, отличающаяся тем, что в нее введен переходный отсек, который вместе с космическим аппаратом и головным обтекателем обеспечивает стыковку с ракетой-носителем, причем стыковочный диаметр головного обтекателя больше стыковочного диаметра последней ступени ракеты-носителя, при этом переходный отсек состоит из нижнего и верхнего усеченных конических корпусов, состыкованных друг с другом по большему диаметру, причем нижний шпангоут нижнего корпуса состыкован с корпусом последней ступени ракеты-носителя, верхний шпангоут верхнего корпуса состыкован с помощью торцевого разъемного, разделяемого в полете, соединения с космическим аппаратом, к верхнему шпангоуту нижнего корпуса пристыкован с помощью торцевого разъемного, разделяемого в полете, соединения головной обтекатель.A space head part comprising a spacecraft and a head fairing, characterized in that a transition compartment is introduced into it, which, together with the spacecraft and the head fairing, provides a docking with a launch vehicle, and the docking diameter of the head fairing is larger than the joint diameter of the last stage of the launch vehicle, wherein the transition compartment consists of the lower and upper truncated conical bodies, joined to each other over a larger diameter, and the lower frame of the lower joint of the joint n with the hull of the last stage of the launch vehicle, the upper frame of the upper body is docked with a split end joint, shared in flight, the spacecraft is docked to the upper frame of the lower body with a split end joint, shared in flight, the head fairing.
Claims (1)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2011132614/11A RU2478531C1 (en) | 2011-08-04 | 2011-08-04 | Spaceship head |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2011132614/11A RU2478531C1 (en) | 2011-08-04 | 2011-08-04 | Spaceship head |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| RU2011132614A true RU2011132614A (en) | 2013-02-10 |
| RU2478531C1 RU2478531C1 (en) | 2013-04-10 |
Family
ID=49119544
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| RU2011132614/11A RU2478531C1 (en) | 2011-08-04 | 2011-08-04 | Spaceship head |
Country Status (1)
| Country | Link |
|---|---|
| RU (1) | RU2478531C1 (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2564458C1 (en) * | 2014-06-26 | 2015-10-10 | Российская Федерация, от имени которой выступает Федеральное космическое агентство | Ascent unit |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6345788B1 (en) * | 1999-05-27 | 2002-02-12 | Trw Inc. | Composite structure element with built-in damping |
| US6622971B1 (en) * | 2001-05-22 | 2003-09-23 | Lockheed Martin Corporation | Adapter for connecting rocket stages |
| RU2179941C1 (en) * | 2001-07-12 | 2002-02-27 | ЗАО "Пусковые услуги" | Space rocket system and method for rendering services in launching space vehicles using space rocket system |
| RU2351510C2 (en) * | 2007-06-01 | 2009-04-10 | Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" имени С.П. Королева" | Space-rocket system |
-
2011
- 2011-08-04 RU RU2011132614/11A patent/RU2478531C1/en not_active IP Right Cessation
Also Published As
| Publication number | Publication date |
|---|---|
| RU2478531C1 (en) | 2013-04-10 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| MM4A | The patent is invalid due to non-payment of fees |
Effective date: 20140805 |