JPS6342855U - - Google Patents
Info
- Publication number
- JPS6342855U JPS6342855U JP13667886U JP13667886U JPS6342855U JP S6342855 U JPS6342855 U JP S6342855U JP 13667886 U JP13667886 U JP 13667886U JP 13667886 U JP13667886 U JP 13667886U JP S6342855 U JPS6342855 U JP S6342855U
- Authority
- JP
- Japan
- Prior art keywords
- solid propellant
- partition wall
- motor case
- solid
- ignites
- 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
- 239000004449 solid propellant Substances 0.000 claims description 11
- 238000005192 partition Methods 0.000 claims description 5
- 239000011810 insulating material Substances 0.000 claims 1
Landscapes
- Toys (AREA)
- Fire-Extinguishing By Fire Departments, And Fire-Extinguishing Equipment And Control Thereof (AREA)
Description
第1図は本考案に係わる固体推進薬ロケツトモ
ータの一実施例を示す縦断側面図、第2図は従来
の固体推進薬ロケツトモータを示す縦断側面図で
ある。
1……モータケース、2……前側固体推進薬、
3……前側点火器、4……タイマ、5……点火用
電池、6……断熱材製仕切壁、7……仕切壁穿孔
用発火器、8……後側点火器、9……後側固体推
進薬、10……ノズル。
FIG. 1 is a longitudinal side view showing an embodiment of a solid propellant rocket motor according to the present invention, and FIG. 2 is a longitudinal side view showing a conventional solid propellant rocket motor. 1... Motor case, 2... Front solid propellant,
3...Front igniter, 4...Timer, 5...Ignition battery, 6...Insulating partition wall, 7...Ignitor for perforating partition wall, 8...Rear igniter, 9...Rear Side solid propellant, 10...nozzle.
Claims (1)
薬を前後複数の固体推進薬に区分する断熱材製仕
切壁と、後側固体推進薬を着火、燃焼させ且つ同
後側固体推進薬の燃焼後所定時間経過してから前
側固体推進薬を着火、燃焼させる点火器とを具え
ていることを特徴とした固体推進薬ロケツトモー
タ。 A motor case, a partition wall made of a heat insulating material that divides the solid propellant in the motor case into a plurality of front and rear solid propellants, and a partition wall that ignites and burns the rear solid propellant, and a predetermined partition wall that separates the solid propellant in the motor case into a plurality of front and rear solid propellants. A solid propellant rocket motor characterized by comprising an igniter that ignites and burns a front solid propellant after a lapse of time.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP13667886U JPS6342855U (en) | 1986-09-08 | 1986-09-08 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP13667886U JPS6342855U (en) | 1986-09-08 | 1986-09-08 |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS6342855U true JPS6342855U (en) | 1988-03-22 |
Family
ID=31040023
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP13667886U Pending JPS6342855U (en) | 1986-09-08 | 1986-09-08 |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS6342855U (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH0278759A (en) * | 1988-08-03 | 1990-03-19 | Morton Thiokol Inc | Solid propellant rocket motor |
JP2012144999A (en) * | 2011-01-07 | 2012-08-02 | Toshiba Corp | Two-pulse flying body |
-
1986
- 1986-09-08 JP JP13667886U patent/JPS6342855U/ja active Pending
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH0278759A (en) * | 1988-08-03 | 1990-03-19 | Morton Thiokol Inc | Solid propellant rocket motor |
JP2012144999A (en) * | 2011-01-07 | 2012-08-02 | Toshiba Corp | Two-pulse flying body |
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