JPS62126544U - - Google Patents
Info
- Publication number
- JPS62126544U JPS62126544U JP1357286U JP1357286U JPS62126544U JP S62126544 U JPS62126544 U JP S62126544U JP 1357286 U JP1357286 U JP 1357286U JP 1357286 U JP1357286 U JP 1357286U JP S62126544 U JPS62126544 U JP S62126544U
- Authority
- JP
- Japan
- Prior art keywords
- nozzle
- combustion chamber
- combustible gas
- intake port
- port cover
- 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
Links
- 238000002485 combustion reaction Methods 0.000 claims description 5
- 239000003380 propellant Substances 0.000 claims description 3
- 238000005192 partition Methods 0.000 description 1
Description
第１図はこの考案の一実施例に基づくラムロケ
ツトを説明する断面図、第２図はポートカバーの
形態を説明する正面図、第３図は閉塞部材が離脱
する状態を説明する隔壁部分の断面図、第４図は
従来におけるラムロケツトの一例を説明する断面
図、第５図は従来におけるポートカバーを説明す
る正面図、第６図は第５図に示すポートカバーの
断面図である。
Ｒ…ラムロケツト、３…二次燃焼室（燃焼室）
、４…デイフユーザ、４ｂ…吸気口、７…サステ
ーナ推進薬、８…ブースタ推進薬、１４…ノズル
、１５…閉塞部材、１６…ポートカバー。
Fig. 1 is a sectional view illustrating a ram rocket based on an embodiment of this invention, Fig. 2 is a front view illustrating the form of the port cover, and Fig. 3 is a sectional view of the partition wall portion illustrating the state in which the closing member is removed. 4 is a sectional view illustrating an example of a conventional ram rocket, FIG. 5 is a front view illustrating a conventional port cover, and FIG. 6 is a sectional view of the port cover shown in FIG. R... Ram rocket, 3... Secondary combustion chamber (combustion chamber)
, 4... Diff user, 4b... Intake port, 7... Sustainer propellant, 8... Booster propellant, 14... Nozzle, 15... Closing member, 16... Port cover.
Claims (1)
ーナ推進薬の燃焼で生じた可燃ガスをノズルから
燃焼室内に噴射すると共に、デイフユーザを介し
て圧縮した空気を吸気口のポートカバーを除去し
て前記燃焼室内に導入し、双方を混合して連続的
に燃焼を行うラムロケツトにおいて、前記ノズル
を吸気口に向けて偏向した状態で設けると共に、
前記ノズルに、当該ノズルを閉塞し且つ可燃ガス
の所定圧力で離脱する際にポートカバーを破壊し
うる衝撃力を付与する閉塞部材を設けたことを特
徴とするラムロケツト。 After starting and accelerating by the booster, the combustible gas generated by the combustion of the sustainer propellant is injected into the combustion chamber from the nozzle, and the compressed air is sent through the diffuser to the combustion chamber by removing the port cover of the intake port. In a ram rocket that mixes the two and continuously burns them, the nozzle is provided with the nozzle deflected toward the intake port, and
A ram rocket characterized in that the nozzle is provided with a closing member that closes the nozzle and applies an impact force capable of destroying the port cover when the combustible gas is released at a predetermined pressure.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP1357286U JPS62126544U (en) | 1986-01-31 | 1986-01-31 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP1357286U JPS62126544U (en) | 1986-01-31 | 1986-01-31 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS62126544U true JPS62126544U (en) | 1987-08-11 |
Family
ID=30802754
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP1357286U Pending JPS62126544U (en) | 1986-01-31 | 1986-01-31 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS62126544U (en) |
-
1986
- 1986-01-31 JP JP1357286U patent/JPS62126544U/ja active Pending
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