JPS62125896U - - Google Patents

Info

Publication number
JPS62125896U
JPS62125896U JP1357186U JP1357186U JPS62125896U JP S62125896 U JPS62125896 U JP S62125896U JP 1357186 U JP1357186 U JP 1357186U JP 1357186 U JP1357186 U JP 1357186U JP S62125896 U JPS62125896 U JP S62125896U
Authority
JP
Japan
Prior art keywords
opening
supply passage
air supply
air intake
control device
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
JP1357186U
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 JP1357186U priority Critical patent/JPS62125896U/ja
Publication of JPS62125896U publication Critical patent/JPS62125896U/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推力方向制
御装置を備えたラムロケツトを説明する断面図、
第2図は第1図に示すラムロケツトの正面図、第
3図は第1図に示すラムロケツトのカバー内部を
説明する拡大断面図、第4図は従来の推力方向制
御装置を備えたラムロケツトを説明する断面図で
ある。 R……ラムロケツト(ロケツト)、N……テー
ルノズル、6a……空気取入れ口、11……空気
供給路、12……電磁バルブ(流量調整手段)。
FIG. 1 is a sectional view illustrating a ram rocket equipped with a thrust direction control device according to an embodiment of the invention;
Fig. 2 is a front view of the ram rocket shown in Fig. 1, Fig. 3 is an enlarged sectional view illustrating the inside of the cover of the ram rocket shown in Fig. 1, and Fig. 4 is an illustration of a ram rocket equipped with a conventional thrust direction control device. FIG. R... Ram rocket (rocket), N... Tail nozzle, 6a... Air intake port, 11... Air supply path, 12... Solenoid valve (flow rate adjustment means).

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 飛翔方向に開口する空気取入れ口と、前記空気
取入れ口に連通し且つテールノズルの内面に開口
する空気供給路と、前記空気供給路を開閉する流
量調整手段とで構成したことを特徴とするロケツ
トの推力方向制御装置。
A rocket characterized by comprising an air intake opening in the flight direction, an air supply passage communicating with the air intake and opening on the inner surface of the tail nozzle, and a flow rate adjustment means for opening and closing the air supply passage. thrust direction control device.
JP1357186U 1986-01-31 1986-01-31 Pending JPS62125896U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP1357186U JPS62125896U (en) 1986-01-31 1986-01-31

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP1357186U JPS62125896U (en) 1986-01-31 1986-01-31

Publications (1)

Publication Number Publication Date
JPS62125896U true JPS62125896U (en) 1987-08-10

Family

ID=30802752

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1357186U Pending JPS62125896U (en) 1986-01-31 1986-01-31

Country Status (1)

Country Link
JP (1) JPS62125896U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH043299U (en) * 1990-04-13 1992-01-13

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH043299U (en) * 1990-04-13 1992-01-13

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