BE860662A - Ensemble de tuyeres perfectionne pour moteur-fusee - Google Patents

Ensemble de tuyeres perfectionne pour moteur-fusee

Info

Publication number
BE860662A
BE860662A BE182497A BE182497A BE860662A BE 860662 A BE860662 A BE 860662A BE 182497 A BE182497 A BE 182497A BE 182497 A BE182497 A BE 182497A BE 860662 A BE860662 A BE 860662A
Authority
BE
Belgium
Prior art keywords
perfected
rocket engine
tip kit
kit
tip
Prior art date
Application number
BE182497A
Other languages
English (en)
French (fr)
Original Assignee
Aerojet General Co
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 Aerojet General Co filed Critical Aerojet General Co
Publication of BE860662A publication Critical patent/BE860662A/xx

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
    • F02K9/08—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/30—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants with the propulsion gases exhausting through a plurality of nozzles
    • 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
    • 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
    • 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
    • Y10S60/00—Power plants
    • Y10S60/909—Reaction motor or component composed of specific material

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)
  • Discharge Of Articles From Conveyors (AREA)
  • Testing Of Engines (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
BE182497A 1977-04-14 1977-11-09 Ensemble de tuyeres perfectionne pour moteur-fusee BE860662A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/787,676 US4150540A (en) 1977-04-14 1977-04-14 Rocket nozzle system

Publications (1)

Publication Number Publication Date
BE860662A true BE860662A (fr) 1978-03-01

Family

ID=25142242

Family Applications (1)

Application Number Title Priority Date Filing Date
BE182497A BE860662A (fr) 1977-04-14 1977-11-09 Ensemble de tuyeres perfectionne pour moteur-fusee

Country Status (5)

Country Link
US (1) US4150540A (xx)
BE (1) BE860662A (xx)
DK (1) DK475977A (xx)
NL (1) NL7712237A (xx)
NO (1) NO774031L (xx)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4577461A (en) * 1983-06-22 1986-03-25 Cann Gordon L Spacecraft optimized arc rocket
US4730449A (en) * 1983-07-26 1988-03-15 Technion, Inc. Radiation transfer thrusters for low thrust applications
DE8908723U1 (de) * 1989-07-18 1989-11-16 Josef Lubig GmbH, 5300 Bonn Düsenbefestigung
KR950007640B1 (ko) * 1992-06-20 1995-07-13 국방과학연구소 로켓트 추진기관의 조립방법
US5359850A (en) * 1993-03-15 1994-11-01 Thiokol Corporation Self venting carbon or graphite phenolic ablatives
US5647201A (en) * 1995-08-02 1997-07-15 Trw Inc. Cavitating venturi for low reynolds number flows
US6330793B1 (en) * 1999-07-02 2001-12-18 Atlantic Research Corporation Erosion resistant rocket nozzle
US7526921B2 (en) * 2005-03-29 2009-05-05 Honeywell International Inc. Auxiliary power unit with integral firebox
WO2011096608A1 (en) * 2010-02-08 2011-08-11 Agency For Defense Development Rocket propulsion device and method for assembling rocket propulsion device
RU2698780C1 (ru) * 2018-08-20 2019-08-29 Акционерное общество "Конструкторское бюро приборостроения им. академика А.Г. Шипунова" Двигательная установка
RU2727116C1 (ru) * 2019-08-22 2020-07-20 Акционерное общество "Конструкторское бюро приборостроения им. академика А.Г. Шипунова" Ракетный двигатель твердого топлива
RU2746081C1 (ru) * 2020-02-11 2021-04-06 Акционерное общество "Опытное конструкторское бюро "Новатор" Вкладыш соплового блока ракетного двигателя твердого топлива из углерод-кремнеземного композиционного материала
CN115506918A (zh) * 2022-08-30 2022-12-23 西安近代化学研究所 一种高推力比三级固体发动机组合装药及燃面设计方法

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3048970A (en) * 1958-10-24 1962-08-14 Stephen H Herzog Plastic nozzle plate for missile motors
US3052090A (en) * 1958-11-20 1962-09-04 Stephen H Herzog Heat shield and nozzle seal for rocket nozzles
US3133411A (en) * 1961-02-23 1964-05-19 Thompson Ramo Wooldridge Inc Rocket nozzle with expandible joints
US3156091A (en) * 1961-07-19 1964-11-10 Curtiss Wright Corp Multi-layer anisotropic heat shield construction
US3285519A (en) * 1964-10-05 1966-11-15 Thiokol Chemical Corp Free expanding displaceable throat insert for a nozzle assembly of a solid propellant rocket motor
US3372548A (en) * 1965-06-17 1968-03-12 Thiokol Chemical Corp Rocket nozzle
US3606164A (en) * 1969-10-23 1971-09-20 Thiokol Chemical Corp Nozzle throat insert assembly
US3771726A (en) * 1970-05-11 1973-11-13 Us Air Force Free-floating rocket nozzle insert
US3694883A (en) * 1970-05-20 1972-10-03 Us Air Force Method of mounting a nozzle insert

Also Published As

Publication number Publication date
NL7712237A (nl) 1978-10-17
DK475977A (da) 1978-10-15
NO774031L (no) 1978-10-17
US4150540A (en) 1979-04-24

Similar Documents

Publication Publication Date Title
SE7812741L (sv) Brenslekomposition
SE7804391L (sv) Forbrenningsmotor for motorfordon
SE7807121L (sv) Byggsats for kabelklemma
DK322578A (da) Smoerende komposition
BR7808509A (pt) Composicao de polimistura
BE863793A (fr) Perfectionnements apportes aux tuyeres des fusees
IT7852137A0 (it) Composizione anti-corrosione
BE860662A (fr) Ensemble de tuyeres perfectionne pour moteur-fusee
IT7867765A0 (it) Calibro per interni
AT359449B (de) Motorzange
SE7806975L (sv) Dieselmotor
BE872573A (fr) Regulateur pour registre
BE866570A (fr) Accessoire pour goulotte
DK148491C (da) Svinefoder
SE7812209L (sv) Forbrenningsenhet
SE7612944L (sv) Tippdrivanordning for konverter
BE867652A (fr) Electrodes de reference pour temperatures elevees
GB2007830B (en) Flare tip
SE7705596L (sv) Forbrenningsforfarande
BE872392A (fr) Fusee de culot
RO75062A (ro) Compozitie de ingrasamint
SE7808948L (sv) Universalmotor
DD132990A1 (de) Drehhubkolben-brennkraftmotor
SE7803333L (sv) Lanshuvud for ferskningslans
FR2384857B1 (fr) Alliage fer-nickel-chrome pour temperatures intermediaires