JPS562444A - Ram rocket - Google Patents

Ram rocket

Info

Publication number
JPS562444A
JPS562444A JP7953079A JP7953079A JPS562444A JP S562444 A JPS562444 A JP S562444A JP 7953079 A JP7953079 A JP 7953079A JP 7953079 A JP7953079 A JP 7953079A JP S562444 A JPS562444 A JP S562444A
Authority
JP
Japan
Prior art keywords
rocket
ram rocket
combustion chamber
motor
ram
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
JP7953079A
Other languages
Japanese (ja)
Inventor
Katsuaki Kosaka
Takuo Kuwabara
Shigeo Iwaki
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 JP7953079A priority Critical patent/JPS562444A/en
Publication of JPS562444A publication Critical patent/JPS562444A/en
Pending legal-status Critical Current

Links

Landscapes

  • Fluidized-Bed Combustion And Resonant Combustion (AREA)

Abstract

PURPOSE: To perform a stable combustion with a spontaneous ignition without using an igniter and flame keeper for a ram rocket, by forming a gas injection port opened almost in perpendicular to an axial line of the ram rocket in a partition that separate primary and secondary combustion chambers of the ram rocket.
CONSTITUTION: A launcher motor not shown in the drawing is mounted to a ram rocket 1 at its rear end and the rocket is accelerated to its necessary flying speed by said motor. And then the lanucher motor is separated to allow the ram rocket 1 to fly in the following manner. That is, gas generating agent 2 is primarily burnt gradually from its end face in a primary combustion chamber 6 to produce inflammable gas at high temperature contg. a large amount of CO, HC and H2 and fill the primary combustion chamber 6 to high pressure. Said inflammable gas is jetted from an injection port 9 into a secondary combustion chamber 7 in the direction almost in perpendicular to an axial line L and diffused in a diffusion area 12. Then it is mixed and fired with air from an air inlet port 11, burnt by passing through a pilot fire keeping area 13 and combustion area 14 and jetted from a nozzle 3.
COPYRIGHT: (C)1981,JPO&Japio
JP7953079A 1979-06-22 1979-06-22 Ram rocket Pending JPS562444A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP7953079A JPS562444A (en) 1979-06-22 1979-06-22 Ram rocket

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP7953079A JPS562444A (en) 1979-06-22 1979-06-22 Ram rocket

Publications (1)

Publication Number Publication Date
JPS562444A true JPS562444A (en) 1981-01-12

Family

ID=13692536

Family Applications (1)

Application Number Title Priority Date Filing Date
JP7953079A Pending JPS562444A (en) 1979-06-22 1979-06-22 Ram rocket

Country Status (1)

Country Link
JP (1) JPS562444A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS52110551A (en) * 1976-03-12 1977-09-16 Toyota Motor Co Ltd Plate glass with antenna with feeder element
CN110566365A (en) * 2019-09-29 2019-12-13 中国人民解放军国防科技大学 Mode-switchable solid combined engine and missile

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS52110551A (en) * 1976-03-12 1977-09-16 Toyota Motor Co Ltd Plate glass with antenna with feeder element
JPS615282B2 (en) * 1976-03-12 1986-02-17 Nippon Ita Garasu Kk
CN110566365A (en) * 2019-09-29 2019-12-13 中国人民解放军国防科技大学 Mode-switchable solid combined engine and missile
CN110566365B (en) * 2019-09-29 2021-01-08 中国人民解放军国防科技大学 Mode-switchable solid combined engine and missile

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