JPS6454199A - Rocket-motor fallaway mechanism - Google Patents
Rocket-motor fallaway mechanismInfo
- Publication number
- JPS6454199A JPS6454199A JP62211888A JP21188887A JPS6454199A JP S6454199 A JPS6454199 A JP S6454199A JP 62211888 A JP62211888 A JP 62211888A JP 21188887 A JP21188887 A JP 21188887A JP S6454199 A JPS6454199 A JP S6454199A
- Authority
- JP
- Japan
- Prior art keywords
- carrier
- airframe
- piston
- solenoid
- pin
- 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
- 238000012544 monitoring process Methods 0.000 abstract 1
Landscapes
- Machine Tool Units (AREA)
Abstract
PURPOSE: To arbitrarily separably provide a rocket motor by constituting to detach a pin from a cutout of a carrier by axially retracting the pin at the time of energizing a solenoid, thereby eliminating a contact of the carrier with an airframe at the time of an unstable state. CONSTITUTION: Since an airframe attitude is frequently changed due to a thrust unbalance immediately after a rocket motor is burned, an energization of a solenoid 5 is executed in a stable state by monitoring the attitude. When the solenoid 5 is energized, a pin 3 with a flange is axially returned and retracted. A carrier 1 is displaced from a front piston 2 by a force of a spring 8, and the piston 2 is retracted into an airframe 15 by a tensile force of a spring 9. After the carrier 1 is displaced out of the piston 2, the carrier 1 is rotated at a rear piston as a center by a force of the detaching spring, and separated from the airframe 15.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP62211888A JPS6454199A (en) | 1987-08-25 | 1987-08-25 | Rocket-motor fallaway mechanism |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP62211888A JPS6454199A (en) | 1987-08-25 | 1987-08-25 | Rocket-motor fallaway mechanism |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS6454199A true JPS6454199A (en) | 1989-03-01 |
Family
ID=16613297
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP62211888A Pending JPS6454199A (en) | 1987-08-25 | 1987-08-25 | Rocket-motor fallaway mechanism |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS6454199A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2007101138A (en) * | 2005-10-07 | 2007-04-19 | Daicel Chem Ind Ltd | Connecting and separating device |
JP2007107796A (en) * | 2005-10-13 | 2007-04-26 | Daicel Chem Ind Ltd | Connection and separation device |
JP2007113826A (en) * | 2005-10-19 | 2007-05-10 | Daicel Chem Ind Ltd | Connecting and separating device |
JP2007120804A (en) * | 2005-10-26 | 2007-05-17 | Daicel Chem Ind Ltd | Connecting and separating device |
CN107976123A (en) * | 2017-11-14 | 2018-05-01 | 南京理工大学 | A kind of shrapnel inertia kinetic energy formula scattering mechanism |
-
1987
- 1987-08-25 JP JP62211888A patent/JPS6454199A/en active Pending
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2007101138A (en) * | 2005-10-07 | 2007-04-19 | Daicel Chem Ind Ltd | Connecting and separating device |
JP2007107796A (en) * | 2005-10-13 | 2007-04-26 | Daicel Chem Ind Ltd | Connection and separation device |
JP2007113826A (en) * | 2005-10-19 | 2007-05-10 | Daicel Chem Ind Ltd | Connecting and separating device |
JP2007120804A (en) * | 2005-10-26 | 2007-05-17 | Daicel Chem Ind Ltd | Connecting and separating device |
CN107976123A (en) * | 2017-11-14 | 2018-05-01 | 南京理工大学 | A kind of shrapnel inertia kinetic energy formula scattering mechanism |
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