FR2165695B1 - - Google Patents

Info

Publication number
FR2165695B1
FR2165695B1 FR7115337A FR7115337A FR2165695B1 FR 2165695 B1 FR2165695 B1 FR 2165695B1 FR 7115337 A FR7115337 A FR 7115337A FR 7115337 A FR7115337 A FR 7115337A FR 2165695 B1 FR2165695 B1 FR 2165695B1
Authority
FR
France
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
Application number
FR7115337A
Other versions
FR2165695A1 (fr
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.)
Hawker Siddeley Dynamics Ltd
Original Assignee
Hawker Siddeley Dynamics 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 Hawker Siddeley Dynamics Ltd filed Critical Hawker Siddeley Dynamics Ltd
Publication of FR2165695A1 publication Critical patent/FR2165695A1/fr
Application granted granted Critical
Publication of FR2165695B1 publication Critical patent/FR2165695B1/fr
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/80—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
    • F02K9/84—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control using movable nozzles

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
FR7115337A 1970-04-30 1971-04-29 Expired FR2165695B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB322570 1970-04-30

Publications (2)

Publication Number Publication Date
FR2165695A1 FR2165695A1 (fr) 1973-08-10
FR2165695B1 true FR2165695B1 (fr) 1976-02-06

Family

ID=9754332

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7115337A Expired FR2165695B1 (fr) 1970-04-30 1971-04-29

Country Status (4)

Country Link
US (1) US3764091A (fr)
FR (1) FR2165695B1 (fr)
GB (1) GB1342342A (fr)
SE (1) SE377719C (fr)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4085909A (en) * 1976-10-04 1978-04-25 Ford Motor Company Combined warm gas fin and reaction control servo
US6568628B1 (en) * 1977-07-28 2003-05-27 Raytheon Company Shipboard point defense system and elements therefor
US4274610A (en) * 1978-07-14 1981-06-23 General Dynamics, Pomona Division Jet tab control mechanism for thrust vector control
US4561357A (en) * 1982-09-15 1985-12-31 General Dynamics Pomona Division Steering mechanism for an explosively fired projectile
FR2635180B1 (fr) * 1988-08-05 1992-11-06 Aris Spa Ensemble de commande, de controle et de propulsion, en particulier pour des objets balistiques
US5125596A (en) * 1989-05-23 1992-06-30 Cavalleri Robert J Fluid shielded movable strut for missile and rocket thrust vector control
JP3710099B2 (ja) * 1995-03-31 2005-10-26 株式会社アイ・エイチ・アイ・エアロスペース ジェッタベータ
US6250584B1 (en) 1999-10-18 2001-06-26 Hr Textron, Inc. Missile fin locking mechanism
SE518657C2 (sv) * 2000-07-03 2002-11-05 Bofors Defence Ab Fenstabiliserad styrbar projektil
US6948685B2 (en) 2003-10-27 2005-09-27 Hr Textron, Inc. Locking device with solenoid release pin
US7262394B2 (en) * 2004-03-05 2007-08-28 The Boeing Company Mortar shell ring tail and associated method
US7195197B2 (en) * 2005-02-11 2007-03-27 Hr Textron, Inc. Techniques for controlling a fin with unlimited adjustment and no backlash
US8362408B2 (en) * 2009-10-22 2013-01-29 Honeywell International Inc. Steerable projectile charging system
FR2970702B1 (fr) * 2011-01-26 2013-05-10 Astrium Sas Procede et systeme de pilotage d'un engin volant a propulseur arriere
CN102363444B (zh) * 2011-09-09 2013-07-17 江西洪都航空工业集团有限责任公司 一种尾翼横向折叠机构
CN104085526B (zh) * 2014-06-25 2016-03-30 西北工业大学 一种实现巡飞器翼身连接、固定、锁死、解锁的一体化结构

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2780059A (en) * 1955-11-29 1957-02-05 Willy A Fiedler Jet direction control device
US3003312A (en) * 1957-08-19 1961-10-10 Thompson Ramo Wooldridge Inc Exhaust nozzle for jet engines
US3210935A (en) * 1959-09-23 1965-10-12 Lyman C Fisher Jetevator for missile control
US3069852A (en) * 1959-10-27 1962-12-25 Goodyear Aircraft Corp Thrust vectoring apparatus
US3210936A (en) * 1959-12-10 1965-10-12 Lyman C Fisher Jetevator for missile control
US3102390A (en) * 1960-03-09 1963-09-03 Fredrick R Barnet Jetevator system design
US3233834A (en) * 1962-07-09 1966-02-08 Aerojet General Co Sealing means for rocket nozzle and jet deflection device mounted thereon
US3285520A (en) * 1964-11-10 1966-11-15 Glenn A Johnson Eccentrically pivoted jetevator with conformable seal
US3438581A (en) * 1967-02-06 1969-04-15 Continental Aviat & Eng Corp Internally gimbaled vectoring nozzle

Also Published As

Publication number Publication date
GB1342342A (en) 1974-01-03
SE377719B (fr) 1975-07-21
FR2165695A1 (fr) 1973-08-10
US3764091A (en) 1973-10-09
SE377719C (sv) 1978-11-20

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Legal Events

Date Code Title Description
TP Transmission of property
ST Notification of lapse