JPH03102048U - - Google Patents
Info
- Publication number
- JPH03102048U JPH03102048U JP1078290U JP1078290U JPH03102048U JP H03102048 U JPH03102048 U JP H03102048U JP 1078290 U JP1078290 U JP 1078290U JP 1078290 U JP1078290 U JP 1078290U JP H03102048 U JPH03102048 U JP H03102048U
- Authority
- JP
- Japan
- Prior art keywords
- rocket motor
- combustion
- combustion chamber
- air intake
- intake port
- 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 9
- 239000007787 solid Substances 0.000 claims description 4
- 239000000567 combustion gas Substances 0.000 claims 2
- 239000003380 propellant Substances 0.000 claims 1
- 239000012212 insulator Substances 0.000 description 1
Description
第1図は、この考案による固体ロケツトモータ
の一実施例の断面図、第2図は従来の固体ロケツ
トモータの断面図である。
図において、1…固体ロケツトモータ、2…空
気取入口、3…圧力センサー、4…空気取入口バ
ルブ、5…バルブ制御装置、6…燃焼室、7…ノ
ズル部、8…ノズル部出口、9…インシユレータ
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 an embodiment of a solid rocket motor according to this invention, and FIG. 2 is a sectional view of a conventional solid rocket motor. In the figure, 1... solid rocket motor, 2... air intake, 3... pressure sensor, 4... air intake valve, 5... valve control device, 6... combustion chamber, 7... nozzle section, 8... nozzle section outlet, 9 ...It is an insulator. In each figure, the same reference numerals indicate the same or corresponding parts.
Claims (1)
られ、燃焼により燃焼ガスを発生する推進薬と、
上記燃焼室の燃焼ガス発生口につながるノズル部
とを具備した固体ロケツトモータにおいて、燃焼
室への空気取入口と、上記空気取入口を開閉でき
、ロケツトモータの燃焼終了後は上記空気取入口
を開くバルブとを有し、ロケツトモータの燃焼終
了後、飛しよう体の慣性飛しよう時における上記
ノズル出口付近に生ずる死水域の低圧部と大気圧
との圧力差を利用し上記空気取入口から空気を取
り入れ燃焼室及びノズル部に空気を流すことによ
りロケツトモータ内部から熱を奪いロケツトモー
タを冷却する機能を備えた固体ロケツトモータ。 A rocket motor combustion chamber, a propellant provided within the combustion chamber and generating combustion gas by combustion,
In a solid rocket motor equipped with a nozzle portion connected to the combustion gas generation port of the combustion chamber, the air intake port to the combustion chamber and the air intake port can be opened and closed, and after the combustion of the rocket motor is completed, the air intake port is closed. After the combustion of the rocket motor is completed, air is released from the air intake port by utilizing the pressure difference between the low pressure part of the dead zone that occurs near the nozzle exit and the atmospheric pressure when the flying object flies due to inertia. A solid-state rocket motor with a function that cools the rocket motor by drawing heat from inside the rocket motor and flowing air through the combustion chamber and nozzle.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP1078290U JPH03102048U (en) | 1990-02-06 | 1990-02-06 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP1078290U JPH03102048U (en) | 1990-02-06 | 1990-02-06 |
Publications (1)
Publication Number | Publication Date |
---|---|
JPH03102048U true JPH03102048U (en) | 1991-10-24 |
Family
ID=31514336
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP1078290U Pending JPH03102048U (en) | 1990-02-06 | 1990-02-06 |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH03102048U (en) |
-
1990
- 1990-02-06 JP JP1078290U patent/JPH03102048U/ja active Pending
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