RU2011132615A - SPACE HEAD - Google Patents
SPACE HEAD Download PDFInfo
- Publication number
- RU2011132615A RU2011132615A RU2011132615/11A RU2011132615A RU2011132615A RU 2011132615 A RU2011132615 A RU 2011132615A RU 2011132615/11 A RU2011132615/11 A RU 2011132615/11A RU 2011132615 A RU2011132615 A RU 2011132615A RU 2011132615 A RU2011132615 A RU 2011132615A
- Authority
- RU
- Russia
- Prior art keywords
- spacecraft
- compartment
- separated
- fairing
- head
- Prior art date
Links
Landscapes
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Laminated Bodies (AREA)
Abstract
Космическая головная часть, состоящая из головного обтекателя и космического аппарата, отличающаяся тем, что в состав космической головной части введен промежуточный отсек, обеспечивающий с помощью разделяемых в полете соединений связь космического аппарата с ракетой-носителем и головным обтекателем, причем агрегатная часть космического аппарата размещена во внутренней полости промежуточного отсека и находится вне пределов зоны схода промежуточного отсека, отделяемого от космического аппарата вместе с ракетой-носителем, а в верхнем шпангоуте промежуточного отсека совмещены два торцевых разъемных соединения, разделяемых в полете, соединяющих этот отсек с головным обтекателем и с космическим аппаратом соответственно.The space head part, consisting of the head fairing and the spacecraft, characterized in that an intermediate compartment is introduced into the space head part, which ensures the communication of the spacecraft with the launch vehicle and the head fairing by means of the connections separated in flight, the aggregate part of the spacecraft being placed in the internal cavity of the intermediate compartment and is located outside the vanishing zone of the intermediate compartment, separated from the spacecraft along with the launch vehicle, and in the upper intermediate bulkhead compartment separable two end compound are combined, separated in flight connecting the compartment with the payload fairing with the spacecraft respectively.
Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2011132615/11A RU2478533C1 (en) | 2011-08-04 | 2011-08-04 | Spaceship head |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2011132615/11A RU2478533C1 (en) | 2011-08-04 | 2011-08-04 | Spaceship head |
Publications (2)
Publication Number | Publication Date |
---|---|
RU2011132615A true RU2011132615A (en) | 2013-02-10 |
RU2478533C1 RU2478533C1 (en) | 2013-04-10 |
Family
ID=49119545
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU2011132615/11A RU2478533C1 (en) | 2011-08-04 | 2011-08-04 | Spaceship head |
Country Status (1)
Country | Link |
---|---|
RU (1) | RU2478533C1 (en) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2555898C2 (en) * | 2013-09-12 | 2015-07-10 | Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" имени С.П. Королева" | Space and missile system |
RU2567981C1 (en) * | 2014-10-01 | 2015-11-10 | Акционерное общество "Ракетно-космический центр "Прогресс" (АО "РКЦ "Прогресс") | Spaceship head |
RU2603872C1 (en) * | 2015-08-06 | 2016-12-10 | Федеральное государственное унитарное предприятие "Научно-производственное объединение им. С.А. Лавочкина" | Transfer compartment of carrier rocket (versions) |
RU2698838C1 (en) * | 2018-04-24 | 2019-08-30 | Акционерное общество "Корпорация "Московский институт теплотехники" (АО "Корпорация "МИТ") | Head of space carrier rocket and method of launching spacecrafts |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2161108C1 (en) * | 2000-02-07 | 2000-12-27 | Государственный космический научно-производственный центр им. М.В. Хруничева | Method for orbit injection of payload by multifunctional launch vehicle of combination arrangement with cruise liquid- propellant rocket engine installations (lrei), multifunctional launch vehicle with cruise lpei and method for its development |
US6622971B1 (en) * | 2001-05-22 | 2003-09-23 | Lockheed Martin Corporation | Adapter for connecting rocket stages |
RU2239585C1 (en) * | 2003-02-21 | 2004-11-10 | Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" им. С.П. Королева" | System for injection of spacecraft |
-
2011
- 2011-08-04 RU RU2011132615/11A patent/RU2478533C1/en not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
RU2478533C1 (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: 20200805 |