JPS6449899A - Guided missile - Google Patents

Guided missile

Info

Publication number
JPS6449899A
JPS6449899A JP20704687A JP20704687A JPS6449899A JP S6449899 A JPS6449899 A JP S6449899A JP 20704687 A JP20704687 A JP 20704687A JP 20704687 A JP20704687 A JP 20704687A JP S6449899 A JPS6449899 A JP S6449899A
Authority
JP
Japan
Prior art keywords
developed
wings
stored
stability
chemical
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
JP20704687A
Other languages
Japanese (ja)
Inventor
Nobuo Kamei
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.)
Mitsubishi Electric Corp
Original Assignee
Mitsubishi Electric 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 Mitsubishi Electric Corp filed Critical Mitsubishi Electric Corp
Priority to JP20704687A priority Critical patent/JPS6449899A/en
Publication of JPS6449899A publication Critical patent/JPS6449899A/en
Pending legal-status Critical Current

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Abstract

PURPOSE: To enable a sufficient performance of motion and aerodynamic stability performance to be attained by a method wherein two kinds of developed wings of a missile are developed after launching by operating a gas cylinder with a pressure of gas of output chemicals and further with a twisting torque stored in a torsion bar after a predetermined delay time. CONSTITUTION: There are provided a steering device stored in an airframe 1, developed steering wings 2 steered by the steering device and a developed stability wing 3 fixed to the airframe 1, wherein both developed wings are stored by a lock device 7 arranged at each of the wings. After launching from a master airplane, a time delaying chemical 19 and an output chemical 20 are ignited by an ignition plug 18 after elapsing a predetermined delay in time, a piston 15 ascends with energy of combustion gas 22 generated by the output chemical 20. When it is pulled out of a hole 16 arranged at the developed stability wing 3, the developed stability wing 3 is developed by a force of the twisting torque stored in a torsion bar through a gear 13.
JP20704687A 1987-08-20 1987-08-20 Guided missile Pending JPS6449899A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP20704687A JPS6449899A (en) 1987-08-20 1987-08-20 Guided missile

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP20704687A JPS6449899A (en) 1987-08-20 1987-08-20 Guided missile

Publications (1)

Publication Number Publication Date
JPS6449899A true JPS6449899A (en) 1989-02-27

Family

ID=16533309

Family Applications (1)

Application Number Title Priority Date Filing Date
JP20704687A Pending JPS6449899A (en) 1987-08-20 1987-08-20 Guided missile

Country Status (1)

Country Link
JP (1) JPS6449899A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2014503400A (en) * 2010-08-03 2014-02-13 サムソン エーアイピー、インク． Retractable wing hinges and trusses for flying vehicles
CN103963960A (en) * 2014-05-14 2014-08-06 北京航空航天大学 Semi-rigid inflatable automatically-unfolded-folded wing
JP2016128322A (en) * 2009-09-09 2016-07-14 エアロバイロメント, インコーポレイテッドAerovironment, Inc. Elevon control system
CN107289822A (en) * 2017-07-19 2017-10-24 贵州航天风华精密设备有限公司 A kind of missile airfoil fold mechanism with multiple rows of torsion bar
CN109050879A (en) * 2018-08-01 2018-12-21 中国航空工业集团公司沈阳飞机设计研究所 A kind of folding support rod formula wingfold mechanism

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2016128322A (en) * 2009-09-09 2016-07-14 エアロバイロメント, インコーポレイテッドAerovironment, Inc. Elevon control system
CN106800085A (en) * 2009-09-09 2017-06-06 威罗门飞行公司 Elevon control system
CN106800085B (en) * 2009-09-09 2020-08-18 威罗门飞行公司 Elevon control system
CN112124563A (en) * 2009-09-09 2020-12-25 威罗门飞行公司 Elevon control system
JP2014503400A (en) * 2010-08-03 2014-02-13 サムソン エーアイピー、インク． Retractable wing hinges and trusses for flying vehicles
CN103963960A (en) * 2014-05-14 2014-08-06 北京航空航天大学 Semi-rigid inflatable automatically-unfolded-folded wing
CN107289822A (en) * 2017-07-19 2017-10-24 贵州航天风华精密设备有限公司 A kind of missile airfoil fold mechanism with multiple rows of torsion bar
CN109050879A (en) * 2018-08-01 2018-12-21 中国航空工业集团公司沈阳飞机设计研究所 A kind of folding support rod formula wingfold mechanism
CN109050879B (en) * 2018-08-01 2021-11-19 中国航空工业集团公司沈阳飞机设计研究所 Folding brace rod type wing folding mechanism

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