BE863793A - Perfectionnements apportes aux tuyeres des fusees - Google Patents

Perfectionnements apportes aux tuyeres des fusees

Info

Publication number
BE863793A
BE863793A BE185023A BE185023A BE863793A BE 863793 A BE863793 A BE 863793A BE 185023 A BE185023 A BE 185023A BE 185023 A BE185023 A BE 185023A BE 863793 A BE863793 A BE 863793A
Authority
BE
Belgium
Prior art keywords
rocket
pipes
rocket pipes
Prior art date
Application number
BE185023A
Other languages
English (en)
Inventor
M N Clark
D L Smith
Original Assignee
Canada Majesty In Right Of
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 Canada Majesty In Right Of filed Critical Canada Majesty In Right Of
Publication of BE863793A publication Critical patent/BE863793A/fr

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
    • F02K9/97—Rocket nozzles
    • F02K9/974—Nozzle- linings; Ablative coatings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/02—Stabilising arrangements
    • F42B10/14—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
    • F42B10/16—Wrap-around fins
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/02—Stabilising arrangements
    • F42B10/26—Stabilising arrangements using spin
    • F42B10/28—Stabilising arrangements using spin induced by gas action
    • F42B10/30—Stabilising arrangements using spin induced by gas action using rocket motor nozzles
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S239/00—Fluid sprinkling, spraying, and diffusing
    • Y10S239/19—Nozzle materials

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Moulding By Coating Moulds (AREA)
  • Lining Or Joining Of Plastics Or The Like (AREA)
  • Laminated Bodies (AREA)
BE185023A 1977-05-25 1978-02-09 Perfectionnements apportes aux tuyeres des fusees BE863793A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CA279,107A CA1079078A (fr) 1977-05-25 1977-05-25 Tuyere de fusee

Publications (1)

Publication Number Publication Date
BE863793A true BE863793A (fr) 1978-05-29

Family

ID=4108728

Family Applications (1)

Application Number Title Priority Date Filing Date
BE185023A BE863793A (fr) 1977-05-25 1978-02-09 Perfectionnements apportes aux tuyeres des fusees

Country Status (12)

Country Link
US (1) US4232843A (fr)
JP (2) JPS53146021A (fr)
BE (1) BE863793A (fr)
CA (1) CA1079078A (fr)
DE (2) DE2807807A1 (fr)
DK (1) DK147559C (fr)
FR (1) FR2392240A1 (fr)
GB (1) GB1593015A (fr)
IT (1) IT1103125B (fr)
NL (1) NL184802C (fr)
NO (1) NO147812C (fr)
SE (1) SE437285B (fr)

Families Citing this family (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA1217944A (fr) * 1983-03-16 1987-02-17 Christian J.L. Carrier Etancheite et organe d'allumage integre pour reacteurs a combustible solide
US4497460A (en) * 1983-03-25 1985-02-05 The United States Of America As Represented By The Secretary Of The Navy Erodale spin turbine for tube-launched missiles
FR2594891B1 (fr) * 1986-02-21 1989-10-13 Poudres & Explosifs Ste Nale Allumeur fixable dans la tuyere d'un propulseur
JPH0710052Y2 (ja) * 1987-09-21 1995-03-08 日産自動車株式会社 ロケットの点火指令伝送装置
FR2630502B1 (fr) * 1988-04-25 1990-08-31 Europ Propulsion Propulseur composite a ailes composites integrees et son procede de fabrication
US5511745A (en) * 1994-12-30 1996-04-30 Thiokol Corporation Vectorable nozzle having jet vanes
GB2308089A (en) * 1995-12-15 1997-06-18 Vic Tree Injection moulding shuttlecock cork
WO1999046499A1 (fr) * 1998-03-10 1999-09-16 Tsai, Artur Tuyere d'ejection a ame rayee
DE19927734C2 (de) * 1999-06-17 2002-04-11 Astrium Gmbh Schubkammer eines Antriebstriebwerks für Satelliten und Transportgeräte für Raumfahrtanwendungen
RU2163686C1 (ru) * 1999-07-21 2001-02-27 Государственное унитарное предприятие "Государственное научно-производственное предприятие "Сплав" Ракетный двигатель твердого топлива
RU2211939C2 (ru) * 2001-04-05 2003-09-10 Федеральное государственное унитарное предприятие Государственный ракетный центр "КБ им. акад. В.П. Макеева" Сопло ракетного двигателя для придания ракете вращения относительно продольной оси
GB0109277D0 (en) * 2001-04-12 2001-05-30 Olympic Technologies Ltd Small arms projectile
GB0111171D0 (en) * 2001-05-08 2001-06-27 Special Cartridge Company Ltd Projictile
US7269951B2 (en) * 2004-09-27 2007-09-18 Honeywell International, Inc. Throat retention apparatus for hot gas applications
RU2272925C1 (ru) * 2004-11-01 2006-03-27 Открытое акционерное общество "Корпорация "Тактическое ракетное вооружение" Заглушка реактивного двигателя
US7918419B2 (en) * 2005-07-15 2011-04-05 Rcs Rocket Motor Components, Inc. Rocket ejection delay apparatus and/or method
WO2007044977A2 (fr) * 2005-10-13 2007-04-19 Raytheon Company Ensemble d'echappement pour systeme d'entrainement d'ejection de matiere
US20100024428A1 (en) * 2006-07-31 2010-02-04 Rosenfield Gary C Rocket Apparatus and/or Method
KR101055669B1 (ko) * 2008-10-30 2011-08-10 국방과학연구소 로켓 추진장치 및 로켓 추진장치 조립방법
WO2011096608A1 (fr) * 2010-02-08 2011-08-11 Agency For Defense Development Dispositif de propulsion de fusée et procédé d'assemblage de dispositif de propulsion de fusée
KR101234218B1 (ko) * 2010-06-25 2013-02-18 국방과학연구소 비행체의 날개장치 및 이를 구비하는 비행체
KR101234179B1 (ko) * 2011-03-21 2013-02-21 김준규 추진 유닛의 회전추력 유도 방법 및 장치
US8826822B1 (en) * 2013-04-23 2014-09-09 Jian-Lin Huang Rocket without tail flame
WO2015075503A1 (fr) * 2013-11-21 2015-05-28 Thor International Sas Tuyère en plastique de propulsion pour roquettes
RU2559657C1 (ru) * 2014-10-01 2015-08-10 Открытое акционерное общество "Научно-производственное объединение "СПЛАВ" Ракетная часть реактивного снаряда
US11469039B2 (en) * 2020-04-09 2022-10-11 Hitachi Energy Switzerland Ag Expandable turret for electrical equipment
CN113237393A (zh) * 2021-04-28 2021-08-10 北京星途探索科技有限公司 一种高精度稳定装置
US12078458B1 (en) * 2023-04-07 2024-09-03 The Boeing Company Fin deployment system for a projectile, projectile, and method of deploying a fin on a projectile

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2645999A (en) * 1947-07-18 1953-07-21 Ben T Bogard Nozzle closure-contact ring assembly for rockets
US3048972A (en) * 1958-01-07 1962-08-14 Ici Ltd Rocket motor construction
FR1229074A (fr) * 1959-04-30 1960-09-02 Etat Francais Represente Par Empennage déployant à plusieurs ailettes mobiles et conjuguées, pour projectiles
US3103784A (en) * 1960-11-15 1963-09-17 Ronald F Vetter Plastic internal rocket nozzle
US3177809A (en) * 1962-07-24 1965-04-13 Budd Co Semi-fixed artillery round
US3196793A (en) * 1963-01-16 1965-07-27 Milenkovic Veljko Folded fin rocket
CH408718A (de) * 1964-02-21 1966-02-28 Oerlikon Buehrle Holding Ag Zündeinrichtung an Raketen
US3648461A (en) * 1970-05-13 1972-03-14 Nasa Solid propellent rocket motor nozzle
US3635404A (en) * 1970-06-18 1972-01-18 Us Navy Spin stabilizing rocket nozzle
US3695556A (en) * 1970-08-03 1972-10-03 Us Navy Hinged stability and control fin assembly
US3952970A (en) * 1974-08-28 1976-04-27 The United States Of America As Represented By The Secretary Of The Navy Means for improving rocket missile accuracy
CA1036419A (fr) * 1975-08-25 1978-08-15 Fred A. Christie Systeme d'allumage arriere pour moteur a propulsion par reaction

Also Published As

Publication number Publication date
DK62678A (da) 1978-11-26
FR2392240A1 (fr) 1978-12-22
IT7848204A0 (it) 1978-02-27
DE2807807A1 (de) 1978-11-30
GB1593015A (en) 1981-07-15
NO147812B (no) 1983-03-07
NO780466L (no) 1978-11-28
IT1103125B (it) 1985-10-14
DE2807807C2 (fr) 1990-01-04
DE7805493U1 (de) 1978-08-24
US4232843A (en) 1980-11-11
NL7802005A (nl) 1978-11-28
NL184802C (nl) 1989-11-01
NO147812C (no) 1983-06-15
SE437285B (sv) 1985-02-18
CA1079078A (fr) 1980-06-10
DK147559C (da) 1985-05-28
JPS53146021A (en) 1978-12-19
DK147559B (da) 1984-10-01
FR2392240B1 (fr) 1983-10-28
JPS59157558U (ja) 1984-10-23
SE7802260L (sv) 1978-11-26

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Legal Events

Date Code Title Description
RE20 Patent expired

Owner name: HER MAJESTY IN RIGHT OF CANADA AS REPRESENTED BY

Effective date: 19980209