JP2522167Y2 - 飛しよう体の推力偏向装置 - Google Patents

飛しよう体の推力偏向装置

Info

Publication number
JP2522167Y2
JP2522167Y2 JP1990039020U JP3902090U JP2522167Y2 JP 2522167 Y2 JP2522167 Y2 JP 2522167Y2 JP 1990039020 U JP1990039020 U JP 1990039020U JP 3902090 U JP3902090 U JP 3902090U JP 2522167 Y2 JP2522167 Y2 JP 2522167Y2
Authority
JP
Japan
Prior art keywords
thrust
nozzle
machine axis
valve
lateral
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.)
Expired - Lifetime
Application number
JP1990039020U
Other languages
English (en)
Japanese (ja)
Other versions
JPH043299U (enrdf_load_html_response
Inventor
輝夫 中西
祥孝 田島
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 Heavy Industries Ltd
Original Assignee
Mitsubishi Heavy Industries Ltd
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 Heavy Industries Ltd filed Critical Mitsubishi Heavy Industries Ltd
Priority to JP1990039020U priority Critical patent/JP2522167Y2/ja
Publication of JPH043299U publication Critical patent/JPH043299U/ja
Application granted granted Critical
Publication of JP2522167Y2 publication Critical patent/JP2522167Y2/ja
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Landscapes

  • Nozzles (AREA)
  • Magnetic Bearings And Hydrostatic Bearings (AREA)
JP1990039020U 1990-04-13 1990-04-13 飛しよう体の推力偏向装置 Expired - Lifetime JP2522167Y2 (ja)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP1990039020U JP2522167Y2 (ja) 1990-04-13 1990-04-13 飛しよう体の推力偏向装置

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP1990039020U JP2522167Y2 (ja) 1990-04-13 1990-04-13 飛しよう体の推力偏向装置

Publications (2)

Publication Number Publication Date
JPH043299U JPH043299U (enrdf_load_html_response) 1992-01-13
JP2522167Y2 true JP2522167Y2 (ja) 1997-01-08

Family

ID=31547545

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1990039020U Expired - Lifetime JP2522167Y2 (ja) 1990-04-13 1990-04-13 飛しよう体の推力偏向装置

Country Status (1)

Country Link
JP (1) JP2522167Y2 (enrdf_load_html_response)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2006508320A (ja) * 2002-11-07 2006-03-09 レイセオン・カンパニー ミサイル制御システムおよび方法

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4384690A (en) 1981-03-06 1983-05-24 The United States Of America As Represented By The Secretary Of The Navy Thrust vector control for large deflection angles

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2536720A1 (fr) * 1982-11-29 1984-06-01 Aerospatiale Systeme pour le pilotage d'un missile au moyen de jets gazeux lateraux et missile comportant un tel systeme
JPS62125896U (enrdf_load_html_response) * 1986-01-31 1987-08-10

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4384690A (en) 1981-03-06 1983-05-24 The United States Of America As Represented By The Secretary Of The Navy Thrust vector control for large deflection angles

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2006508320A (ja) * 2002-11-07 2006-03-09 レイセオン・カンパニー ミサイル制御システムおよび方法

Also Published As

Publication number Publication date
JPH043299U (enrdf_load_html_response) 1992-01-13

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