JPS56113032A - Ram rocket - Google Patents

Ram rocket

Info

Publication number
JPS56113032A
JPS56113032A JP1616180A JP1616180A JPS56113032A JP S56113032 A JPS56113032 A JP S56113032A JP 1616180 A JP1616180 A JP 1616180A JP 1616180 A JP1616180 A JP 1616180A JP S56113032 A JPS56113032 A JP S56113032A
Authority
JP
Japan
Prior art keywords
injector
baffle plate
nozzle
combustion chamber
secondary combustion
Prior art date
Legal status (The legal status 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 status listed.)
Pending
Application number
JP1616180A
Other languages
Japanese (ja)
Inventor
Takuo Kuwabara
Katsuaki Kosaka
Shinji Notake
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Nissan Motor Co Ltd
Original Assignee
Nissan Motor Co Ltd
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 Nissan Motor Co Ltd filed Critical Nissan Motor Co Ltd
Priority to JP1616180A priority Critical patent/JPS56113032A/en
Publication of JPS56113032A publication Critical patent/JPS56113032A/en
Pending legal-status Critical Current

Links

Abstract

PURPOSE: To miniaturize a ram rocket itself by arranging a baffle plate which surrounds an injector, forming the ignition source keeping range for combustible gas, and forming the air blowing port for a diffuser in the vicinity of a nozzle.
CONSTITUTION: A metal baffle plate 27 is mounted on a nozzle 13, between an injector 22 and an air blowing port 26, cylindrically surrounding the injector 22, thus the ignition source keeping range 28 for the secondary combustion chamber is formed. A part of the combustible gas collides with the baffle plate 27 and stagnates in the ignition source keeping range 28 between the baffle plate 27 and the injector 22, and flame is kept. While, into the secondary combustion chamber 15, the outside air which is taken-in from an air taking port 25 is blown and mixed with combustible gas, and the gas is perfectly combusted in the secondary combustion chamber 15. Therefore, the air blowing port 26 can be formed in the vicinity of the nozzle 13, and the length of a ram rocket can be shortened.
COPYRIGHT: (C)1981,JPO&Japio
JP1616180A 1980-02-12 1980-02-12 Ram rocket Pending JPS56113032A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP1616180A JPS56113032A (en) 1980-02-12 1980-02-12 Ram rocket

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP1616180A JPS56113032A (en) 1980-02-12 1980-02-12 Ram rocket

Publications (1)

Publication Number Publication Date
JPS56113032A true JPS56113032A (en) 1981-09-05

Family

ID=11908777

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1616180A Pending JPS56113032A (en) 1980-02-12 1980-02-12 Ram rocket

Country Status (1)

Country Link
JP (1) JPS56113032A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR100499797B1 (en) * 2002-11-25 2005-07-07 한국항공우주연구원 Engine of rocket

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR100499797B1 (en) * 2002-11-25 2005-07-07 한국항공우주연구원 Engine of rocket

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