JPS62126545U - - Google Patents

Info

Publication number
JPS62126545U
JPS62126545U JP1357486U JP1357486U JPS62126545U JP S62126545 U JPS62126545 U JP S62126545U JP 1357486 U JP1357486 U JP 1357486U JP 1357486 U JP1357486 U JP 1357486U JP S62126545 U JPS62126545 U JP S62126545U
Authority
JP
Japan
Prior art keywords
ram rocket
diffuser
combustion
sustainer propellant
combustion chamber
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
JP1357486U
Other languages
Japanese (ja)
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 filed Critical
Priority to JP1357486U priority Critical patent/JPS62126545U/ja
Publication of JPS62126545U publication Critical patent/JPS62126545U/ja
Pending legal-status Critical Current

Links

Description

【図面の簡単な説明】[Brief explanation of the drawing]

第1図はこの考案の一実施例によるラムロケツ
トの要部を説明する断面図、第2図は従来におけ
るラムロケツトを説明する部分破断の断面図であ
る。 R…ラムロケツト、3…サステーナ推進薬用燃
焼室、4…主燃焼室、5…デイフユーザ、7…サ
ステーナ推進薬、9…噴出ノズル。
FIG. 1 is a sectional view illustrating the main parts of a ram rocket according to an embodiment of the invention, and FIG. 2 is a partially broken sectional view illustrating a conventional ram rocket. R... Ram rocket, 3... Sustainer propellant combustion chamber, 4... Main combustion chamber, 5... Diffuser, 7... Sustainer propellant, 9... Ejection nozzle.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] サステーナ推進薬の燃焼で生じた可燃ガスとデ
イフユーザを介して圧縮導入した外気とを混合し
て主燃焼室で燃焼を行うラムロケツトにおいて、
前記サステーナ推進薬を装填したサステーナ推進
薬用燃焼室の尾部に、当該ラムロケツトの略半径
方向に開口してデイフユーザに連通する可燃ガス
の噴出ノズルを設けたことを特徴とするラムロケ
ツト。
In a ram rocket, combustion is performed in the main combustion chamber by mixing combustible gas generated by the combustion of sustainer propellant with outside air compressed and introduced through a diffuser.
A ram rocket, characterized in that a combustible gas ejection nozzle is provided at the tail portion of the sustainer propellant combustion chamber loaded with the sustainer propellant, which opens in a substantially radial direction of the ram rocket and communicates with a diffuser.
JP1357486U 1986-01-31 1986-01-31 Pending JPS62126545U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP1357486U JPS62126545U (en) 1986-01-31 1986-01-31

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP1357486U JPS62126545U (en) 1986-01-31 1986-01-31

Publications (1)

Publication Number Publication Date
JPS62126545U true JPS62126545U (en) 1987-08-11

Family

ID=30802758

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1357486U Pending JPS62126545U (en) 1986-01-31 1986-01-31

Country Status (1)

Country Link
JP (1) JPS62126545U (en)

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