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RU2011135260A - METHOD FOR COOLING THE ROCKET HOUSING - Google Patents

METHOD FOR COOLING THE ROCKET HOUSING Download PDF

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Publication number
RU2011135260A
RU2011135260A RU2011135260/11A RU2011135260A RU2011135260A RU 2011135260 A RU2011135260 A RU 2011135260A RU 2011135260/11 A RU2011135260/11 A RU 2011135260/11A RU 2011135260 A RU2011135260 A RU 2011135260A RU 2011135260 A RU2011135260 A RU 2011135260A
Authority
RU
Russia
Prior art keywords
cooling
rocket
air stream
rocket housing
unwound
Prior art date
Application number
RU2011135260/11A
Other languages
Russian (ru)
Other versions
RU2568971C2 (en
Inventor
Александр Борисович Моисеев
Original Assignee
Александр Борисович Моисеев
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.)
Filing date
Publication date
Application filed by Александр Борисович Моисеев filed Critical Александр Борисович Моисеев
Priority to RU2011135260/11A priority Critical patent/RU2568971C2/en
Publication of RU2011135260A publication Critical patent/RU2011135260A/en
Application granted granted Critical
Publication of RU2568971C2 publication Critical patent/RU2568971C2/en

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  • Moulding By Coating Moulds (AREA)

Abstract

Способ охлаждения корпуса движущейся ракеты путем формирования сужающегося в направлении ее движения вихревого воздушного потока при посредстве раскручивающихся от потока воздуха закрепленных на обруче лопастей, причем их вращение осуществляется вокруг внешней поверхности корпуса ракеты.The method of cooling the body of a moving rocket by forming a vortex air stream tapering in the direction of its movement by means of blades fixed on a hoop that are unwound from the air stream, and their rotation is carried out around the outer surface of the rocket body.

Claims (1)

Способ охлаждения корпуса движущейся ракеты путем формирования сужающегося в направлении ее движения вихревого воздушного потока при посредстве раскручивающихся от потока воздуха закрепленных на обруче лопастей, причем их вращение осуществляется вокруг внешней поверхности корпуса ракеты. The method of cooling the body of a moving rocket by forming a vortex air stream tapering in the direction of its movement by means of blades fixed on a hoop that are unwound from the air stream, and their rotation is carried out around the outer surface of the rocket body.
RU2011135260/11A 2011-08-23 2011-08-23 Rocket body cooling process RU2568971C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2011135260/11A RU2568971C2 (en) 2011-08-23 2011-08-23 Rocket body cooling process

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2011135260/11A RU2568971C2 (en) 2011-08-23 2011-08-23 Rocket body cooling process

Publications (2)

Publication Number Publication Date
RU2011135260A true RU2011135260A (en) 2013-03-10
RU2568971C2 RU2568971C2 (en) 2015-11-20

Family

ID=49123043

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2011135260/11A RU2568971C2 (en) 2011-08-23 2011-08-23 Rocket body cooling process

Country Status (1)

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RU (1) RU2568971C2 (en)

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2225330C1 (en) * 2002-08-23 2004-03-10 Федеральное государственное унитарное предприятие "Государственный космический научно-производственный центр им. М.В. Хруничева" Method of thermal protection of flying vehicle and device for realization of this method

Also Published As

Publication number Publication date
RU2568971C2 (en) 2015-11-20

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Legal Events

Date Code Title Description
HE9A Changing address for correspondence with an applicant
MM4A The patent is invalid due to non-payment of fees

Effective date: 20151024