BE810074A - Tuyere extensible pour moteur a fusee ou analogue - Google Patents

Tuyere extensible pour moteur a fusee ou analogue

Info

Publication number
BE810074A
BE810074A BE140104A BE140104A BE810074A BE 810074 A BE810074 A BE 810074A BE 140104 A BE140104 A BE 140104A BE 140104 A BE140104 A BE 140104A BE 810074 A BE810074 A BE 810074A
Authority
BE
Belgium
Prior art keywords
similar
rocket motor
extensible nozzle
extensible
nozzle
Prior art date
Application number
BE140104A
Other languages
English (en)
French (fr)
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 filed Critical
Publication of BE810074A publication Critical patent/BE810074A/xx

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/97Rocket nozzles
    • F02K9/976Deployable nozzles

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Toys (AREA)
BE140104A 1973-02-15 1974-01-23 Tuyere extensible pour moteur a fusee ou analogue BE810074A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/329,909 US3951342A (en) 1973-02-15 1973-02-15 Extendible nozzle for a rocket motor or the like

Publications (1)

Publication Number Publication Date
BE810074A true BE810074A (fr) 1974-05-16

Family

ID=23287540

Family Applications (1)

Application Number Title Priority Date Filing Date
BE140104A BE810074A (fr) 1973-02-15 1974-01-23 Tuyere extensible pour moteur a fusee ou analogue

Country Status (9)

Country Link
US (1) US3951342A (it)
JP (1) JPS49112400A (it)
AU (1) AU6553574A (it)
BE (1) BE810074A (it)
BR (1) BR7400639D0 (it)
DE (1) DE2406535A1 (it)
FR (1) FR2217558A1 (it)
IT (1) IT1002931B (it)
NL (1) NL7402124A (it)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2422831A1 (fr) * 1978-02-03 1979-11-09 Aerospatiale Tuyere de propulseur a divergent deployable
FR2457390A1 (fr) * 1979-05-23 1980-12-19 Europ Propulsion Divergent deployable de tuyere pour propulseur fusee
US4313567A (en) * 1979-12-03 1982-02-02 Rockwell International Corporation Cam-lock rocket securing mechanism
US4706886A (en) * 1984-08-27 1987-11-17 Rockwell International Corporation Extendible rocket-engine nozzle
US4779799A (en) * 1987-03-16 1988-10-25 Rockwell International Corporation Extendible nozzle
RU2455517C1 (ru) * 2011-03-02 2012-07-10 Открытое акционерное общество Научно-производственное объединение "Искра" Сопло переменной степени расширения
US10094646B2 (en) * 2015-04-13 2018-10-09 The Boeing Company Spring-assisted deployment of a pivotable rocket motor
CN112211747A (zh) * 2020-10-13 2021-01-12 西北工业大学 旋转加速型固体火箭发动机内部结构
CN114962079B (zh) * 2022-08-01 2022-11-15 北京凌空天行科技有限责任公司 一种火箭喷管延长结构

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3249306A (en) * 1962-09-14 1966-05-03 Aerojet General Co Automatically adjustable rocket nozzle
US3146669A (en) * 1962-10-24 1964-09-01 Calvin J Wolf Collapsible nozzle exit cone for tube launched missile
US3270504A (en) * 1965-07-20 1966-09-06 Donald R Ward Automatically deploying nozzle exit cone extension
FR1495579A (fr) * 1966-08-09 1967-09-22 Soc Tech De Rech Ind Perfectionnements aux empennages déployants pour projectiles

Also Published As

Publication number Publication date
US3951342A (en) 1976-04-20
FR2217558A1 (it) 1974-09-06
JPS49112400A (it) 1974-10-25
BR7400639D0 (pt) 1974-12-03
DE2406535A1 (de) 1974-09-05
IT1002931B (it) 1976-05-20
AU6553574A (en) 1975-08-14
NL7402124A (it) 1974-08-19

Similar Documents

Publication Publication Date Title
FR2280876A1 (fr) Charge fumigene ejectable pour projectiles fortement sollicites
FR2281506A1 (fr) Support d'injecteur pour moteurs a injection directe
BE836373A (fr) Cloison pour propulseur de fusee
BE810074A (fr) Tuyere extensible pour moteur a fusee ou analogue
BE813531A (fr) Tete d'ejection a charges actives pour fusees
CA965967A (en) Tunnel liners
BE832800A (fr) Amorce de tete autodestructrice pour projectiles giratoires
CA989978A (en) Apparatus for determining the gross thrust of a jet engine
SE427385B (sv) Projektil med ferdrojd sprengverkan
IT954661B (it) Composizione refrattaria applica bile a spruzzo
BE786523A (fr) Tete pour projectile a charge creuse
CA966964A (en) Wax injection nozzle
CA1020346A (en) Preheated air injection device for tunnel furnace
BE806877A (fr) Allumeur a percussion pour projectiles
IT1023880B (it) Giunto autoallineante per gruppi telescopici a funzionamento idrau lic
IL44465A0 (en) External combustion engine
CA1021434A (en) Injection molding machine controls
IL39523A (en) Rocket engine
BE784745A (fr) Compositions pour le moulage d'articles resistant a l'inflammation
BE777622A (fr) Distributeur d'allumage pour moteurs a explosion
AR196309A1 (es) Cohete con cabeza explosiva retractil
BE817555A (fr) Bague d'ejection
FR2334086A1 (fr) Fusee d'amorcage d'obus
IT1025672B (it) Insieme di giunto per albero
BE784957A (fr) Perfectionnements a ou se rapportant a un lisere pour rideaux