NO774031L - Rakettdysesystem. - Google Patents

Rakettdysesystem.

Info

Publication number
NO774031L
NO774031L NO774031A NO774031A NO774031L NO 774031 L NO774031 L NO 774031L NO 774031 A NO774031 A NO 774031A NO 774031 A NO774031 A NO 774031A NO 774031 L NO774031 L NO 774031L
Authority
NO
Norway
Prior art keywords
neck
nozzle
nozzles
rocket
nozzle system
Prior art date
Application number
NO774031A
Other languages
English (en)
Norwegian (no)
Inventor
Harold A Krayenbuhl
Gene Dolgonas
Charles J Rogers
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 NO774031L publication Critical patent/NO774031L/no

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
    • F02K9/08Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/30Rocket-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
    • 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
    • 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
    • F02K9/974Nozzle- linings; Ablative coatings
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S60/00Power plants
    • Y10S60/909Reaction 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)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Discharge Of Articles From Conveyors (AREA)
  • Testing Of Engines (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
NO774031A 1977-04-14 1977-11-24 Rakettdysesystem. NO774031L (no)

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
NO774031L true NO774031L (no) 1978-10-17

Family

ID=25142242

Family Applications (1)

Application Number Title Priority Date Filing Date
NO774031A NO774031L (no) 1977-04-14 1977-11-24 Rakettdysesystem.

Country Status (5)

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

Families Citing this family (15)

* 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
USH408H (en) 1986-04-28 1988-01-05 The United States Of America As Represented By The Secretary Of The Navy Graphite chamber manufacturing process
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 (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
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
CN115506918B (zh) * 2022-08-30 2024-08-02 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
CN119754967B (zh) * 2024-12-11 2025-09-30 西北工业大学 一种喉栓式喷管推力系数计算方法及测试系统

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
US4150540A (en) 1979-04-24
NL7712237A (nl) 1978-10-17
DK475977A (da) 1978-10-15
BE860662A (fr) 1978-03-01

Similar Documents

Publication Publication Date Title
NO774031L (no) Rakettdysesystem.
US5600946A (en) Solid propellant dual pulse rocket motor loaded case and ignition system and method of manufacture
US4084512A (en) Pressure relief construction for controlled combustion of ordnance items
US4574700A (en) Solid rocket motor with nozzle containing aromatic amide fibers
NO147812B (no) Rakettdyseenhet, samt fremgangsmaate for fremstilling av denne
CN110425058B (zh) 双脉冲固体火箭发动机软质隔层烧蚀试验装置
CA1235582A (fr) Moteur fusee a propergol solide a double poussee interrompue
US3698321A (en) Rocket assisted projectile
US4041869A (en) Cook-off liner component
US2773448A (en) Rocket projectile
US5784877A (en) Rocket-ramjet engine casing port closure
CN1302353A (zh) 带外套、充排系统、冷却装置和挂架的模块式固体燃料火箭推进剂装药
US5419119A (en) High pressure slab motor
KR20230082765A (ko) 시험용 추진기관
US3300142A (en) Rocket nozzle capable of inducing flow separation
NO321831B1 (no) Motor med fast drivmiddel og lav folsomhet
RU2189483C2 (ru) Ракетный двигатель твердого топлива
Ostrander et al. Air Turbo-Rocket solid propellant development and testing
Dahl et al. Demonstration of solid propellant pulse motor technologies
US3015209A (en) Means for supporting a propellant charge in a rocket motor
US3026674A (en) Solid propellant rocket motor
RU2110694C1 (ru) Ракетный двигатель твердого топлива
RU2303153C2 (ru) Заряд твердого топлива для ракетного двигателя
US3070958A (en) Programmed output energy solid fuel gas genenrator
US2980021A (en) Ignition of solid rocket propellants