FR2456217A1 - Moteur-fusee - Google Patents

Moteur-fusee

Info

Publication number
FR2456217A1
FR2456217A1 FR8010581A FR8010581A FR2456217A1 FR 2456217 A1 FR2456217 A1 FR 2456217A1 FR 8010581 A FR8010581 A FR 8010581A FR 8010581 A FR8010581 A FR 8010581A FR 2456217 A1 FR2456217 A1 FR 2456217A1
Authority
FR
France
Prior art keywords
rocket
motor
solid propergol
fragment
neck
Prior art date
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.)
Granted
Application number
FR8010581A
Other languages
English (en)
Other versions
FR2456217B1 (fr
Inventor
Wallace Averell Hurd Jr
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.)
Raytheon Co
Original Assignee
Raytheon 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 Raytheon Co filed Critical Raytheon Co
Publication of FR2456217A1 publication Critical patent/FR2456217A1/fr
Application granted granted Critical
Publication of FR2456217B1 publication Critical patent/FR2456217B1/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
    • F02K9/08—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/10—Shape or structure of solid propellant charges
    • F02K9/14—Shape or structure of solid propellant charges made from sheet-like materials, e.g. of carpet-roll type, of layered structure
    • 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
    • F02K9/32—Constructional parts; Details not otherwise provided for

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Testing Of Engines (AREA)
  • Solid Fuels And Fuel-Associated Substances (AREA)
  • Emergency Lowering Means (AREA)
  • Cylinder Crankcases Of Internal Combustion Engines (AREA)
  • Lubrication Details And Ventilation Of Internal Combustion Engines (AREA)
  • Solid-Fuel Combustion (AREA)

Abstract

CE MOTEUR-FUSEE A PROPERGOL SOLIDE COMPREND UN ELEMENT PERFORE 10 DE PROTECTION DISPOSE ENTRE LA CHAMBRE DE COMBUSTION ET LA TUYERE 20 AFIN D'EMPECHER TOUT FRAGMENT 16B DU PROPERGOL SOLIDE NON BRULE DE PENETRER DANS LE COL DE LA TUYERE EN COURS DE FONCTIONNEMENT.
FR8010581A 1979-05-11 1980-05-12 Moteur-fusee Expired FR2456217B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/038,366 US4311005A (en) 1979-05-11 1979-05-11 Rocket motor

Publications (2)

Publication Number Publication Date
FR2456217A1 true FR2456217A1 (fr) 1980-12-05
FR2456217B1 FR2456217B1 (fr) 1985-08-30

Family

ID=21899527

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8010581A Expired FR2456217B1 (fr) 1979-05-11 1980-05-12 Moteur-fusee

Country Status (7)

Country Link
US (1) US4311005A (fr)
JP (1) JPS6053779B2 (fr)
CA (1) CA1134626A (fr)
CH (1) CH645955A5 (fr)
DE (1) DE3017308A1 (fr)
FR (1) FR2456217B1 (fr)
GB (1) GB2049891B (fr)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3507892A1 (de) * 1985-03-06 1986-09-11 Rheinmetall GmbH, 4000 Düsseldorf Gasgenerator
FR2652125B1 (fr) * 1989-09-19 1992-01-10 Europ Agence Spatiale Allumeur consumable pour moteur-fusee a perpergol solide.
US5440993A (en) * 1990-12-07 1995-08-15 Osofsky; Irving B. High velocity impulse rocket
US7360355B1 (en) 1996-06-07 2008-04-22 Qinetiq Limited Long range artillery shell
US8051640B2 (en) * 2008-05-09 2011-11-08 Robert L Geisler Propulsion system, opposing grains rocket engine, and method for controlling the burn rate of solid propellant grains
CN104696104B (zh) * 2013-12-10 2016-08-31 上海新力动力设备研究所 固体火箭发动机挡环连接结构

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2503270A (en) * 1944-11-16 1950-04-11 Clarence N Hickman Trap for rocket propellants
GB664674A (en) * 1949-07-25 1952-01-09 Edward Whitworth Improvements in or relating to devices for delivering under relatively diminished pressure gaseous products of combustion at high pressures of self-combustible solid fuels
FR1008191A (fr) * 1949-01-17 1952-05-14 Fu R Die Entwicklung Von Erfin Projectile
FR1020238A (fr) * 1950-06-15 1953-02-03 Soc Tech De Rech Ind Perfectionnements aux réacteurs à poudre
FR1095546A (fr) * 1953-12-10 1955-06-03 Soc Tech De Rech Ind Propulseur
GB739417A (en) * 1953-03-14 1955-10-26 Energa Improvements in rocket motors
US2958185A (en) * 1952-11-13 1960-11-01 Aerojet General Co Pressure responsive safety device for jet propulsion motors

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US694295A (en) * 1899-08-24 1902-02-25 Hudson Maxim Cartridge.
US952538A (en) * 1904-10-14 1910-03-22 Soc D La Poudre Peigne Et Des Brevets Jacques Luciani Manufacture of gunpowder.
FR1268781A (fr) * 1960-09-26 1961-08-04 Olin Mathieson Moteur de fusée et procédé de réglage de la poussée d'un moteur de fusée
BE793617A (fr) * 1972-02-02 1973-05-02 Diehl Dispositif de surete adapte a des projectiles explosifs
FR2183591B1 (fr) * 1972-05-12 1974-07-26 France Etat

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2503270A (en) * 1944-11-16 1950-04-11 Clarence N Hickman Trap for rocket propellants
FR1008191A (fr) * 1949-01-17 1952-05-14 Fu R Die Entwicklung Von Erfin Projectile
GB664674A (en) * 1949-07-25 1952-01-09 Edward Whitworth Improvements in or relating to devices for delivering under relatively diminished pressure gaseous products of combustion at high pressures of self-combustible solid fuels
FR1020238A (fr) * 1950-06-15 1953-02-03 Soc Tech De Rech Ind Perfectionnements aux réacteurs à poudre
US2958185A (en) * 1952-11-13 1960-11-01 Aerojet General Co Pressure responsive safety device for jet propulsion motors
GB739417A (en) * 1953-03-14 1955-10-26 Energa Improvements in rocket motors
FR1095546A (fr) * 1953-12-10 1955-06-03 Soc Tech De Rech Ind Propulseur

Also Published As

Publication number Publication date
US4311005A (en) 1982-01-19
DE3017308A1 (de) 1980-11-27
JPS6053779B2 (ja) 1985-11-27
JPS55151140A (en) 1980-11-25
CH645955A5 (de) 1984-10-31
GB2049891A (en) 1980-12-31
FR2456217B1 (fr) 1985-08-30
CA1134626A (fr) 1982-11-02
GB2049891B (en) 1983-04-27

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Legal Events

Date Code Title Description
ST Notification of lapse