JPH0285300U - - Google Patents

Info

Publication number
JPH0285300U
JPH0285300U JP16320588U JP16320588U JPH0285300U JP H0285300 U JPH0285300 U JP H0285300U JP 16320588 U JP16320588 U JP 16320588U JP 16320588 U JP16320588 U JP 16320588U JP H0285300 U JPH0285300 U JP H0285300U
Authority
JP
Japan
Prior art keywords
extension tube
rocket motor
motor extension
heat insulating
insulating layer
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
JP16320588U
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 JP16320588U priority Critical patent/JPH0285300U/ja
Publication of JPH0285300U publication Critical patent/JPH0285300U/ja
Pending legal-status Critical Current

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  • Laminated Bodies (AREA)

Description

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

第1図はこの考案の一実施例を示すロケツトモ
ータ延長管の断面図、第2図は従来のロケツトモ
ータ延長管の断面図である。 図において、1は飛しよう体外殻、2はロケツ
トモータ本体、3は高温ガス、4は延長管、5は
操舵装置、6は断熱材、7は操舵翼、8は中空断
熱層である。なお、各図中同一符号は同一または
相当部分を示す。
FIG. 1 is a sectional view of a rocket motor extension tube showing an embodiment of this invention, and FIG. 2 is a sectional view of a conventional rocket motor extension tube. In the figure, 1 is the outer shell of the flying body, 2 is the rocket motor body, 3 is high-temperature gas, 4 is an extension tube, 5 is a steering device, 6 is a heat insulating material, 7 is a steering blade, and 8 is a hollow heat insulating layer. Note that the same reference numerals in each figure indicate the same or corresponding parts.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 後翼操舵型飛しよう体に用いられるロケツトモ
ータ延長管の内周と外周との間に中空断熱層を備
えたことを特徴とするロケツトモータ延長管。
A rocket motor extension tube for use in a rear wing steering type flying object, characterized in that a hollow heat insulating layer is provided between the inner periphery and the outer periphery of the rocket motor extension tube.
JP16320588U 1988-12-16 1988-12-16 Pending JPH0285300U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP16320588U JPH0285300U (en) 1988-12-16 1988-12-16

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP16320588U JPH0285300U (en) 1988-12-16 1988-12-16

Publications (1)

Publication Number Publication Date
JPH0285300U true JPH0285300U (en) 1990-07-04

Family

ID=31447722

Family Applications (1)

Application Number Title Priority Date Filing Date
JP16320588U Pending JPH0285300U (en) 1988-12-16 1988-12-16

Country Status (1)

Country Link
JP (1) JPH0285300U (en)

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