JPS6454199A - Rocket-motor fallaway mechanism - Google Patents

Rocket-motor fallaway mechanism

Info

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
Application number
JP62211888A
Other languages
Japanese (ja)
Inventor
Nozomi Chisaki
Kazuyoshi Sekigawa
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
NEC Corp
Original Assignee
NEC Corp
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 by NEC Corp filed Critical NEC Corp
Priority to JP62211888A priority Critical patent/JPS6454199A/en
Publication of JPS6454199A publication Critical patent/JPS6454199A/en
Pending legal-status Critical Current

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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.
JP62211888A 1987-08-25 1987-08-25 Rocket-motor fallaway mechanism Pending JPS6454199A (en)

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)

* Cited by examiner, † Cited by third party
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

Cited By (5)

* Cited by examiner, † Cited by third party
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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