BE862427A - Dispositif pour la liaison entre deux etages d'un engin autopropulse - Google Patents

Dispositif pour la liaison entre deux etages d'un engin autopropulse

Info

Publication number
BE862427A
BE862427A BE183931A BE183931A BE862427A BE 862427 A BE862427 A BE 862427A BE 183931 A BE183931 A BE 183931A BE 183931 A BE183931 A BE 183931A BE 862427 A BE862427 A BE 862427A
Authority
BE
Belgium
Prior art keywords
stages
self
connection
propelled machine
propelled
Prior art date
Application number
BE183931A
Other languages
English (en)
Original Assignee
Luchaire Sa
Poudres & Explosifs Ste Nale
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 Luchaire Sa, Poudres & Explosifs Ste Nale filed Critical Luchaire Sa
Publication of BE862427A publication Critical patent/BE862427A/fr

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
    • F42B15/36—Means for interconnecting rocket-motor and body section; Multi-stage connectors; Disconnecting means
    • 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
    • F02K9/20—Shape or structure of solid propellant charges of the external-burning type
    • 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
    • F02K9/74—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof combined with another jet-propulsion plant
    • F02K9/76—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof combined with another jet-propulsion plant with another rocket-engine plant; Multistage rocket-engine plants
    • F02K9/763—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof combined with another jet-propulsion plant with another rocket-engine plant; Multistage rocket-engine plants with solid propellant
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Air Bags (AREA)
  • Platform Screen Doors And Railroad Systems (AREA)
BE183931A 1976-12-28 1977-12-28 Dispositif pour la liaison entre deux etages d'un engin autopropulse BE862427A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7639278A FR2376300A1 (fr) 1976-12-28 1976-12-28 Dispositif pour la liaison entre deux etages d'un engin autopropulse

Publications (1)

Publication Number Publication Date
BE862427A true BE862427A (fr) 1978-06-28

Family

ID=9181617

Family Applications (1)

Application Number Title Priority Date Filing Date
BE183931A BE862427A (fr) 1976-12-28 1977-12-28 Dispositif pour la liaison entre deux etages d'un engin autopropulse

Country Status (7)

Country Link
US (1) US4250705A (fr)
BE (1) BE862427A (fr)
DE (1) DE2757806C2 (fr)
FR (1) FR2376300A1 (fr)
GB (1) GB1543690A (fr)
IT (1) IT1091528B (fr)
SE (1) SE421831B (fr)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3412701C2 (de) * 1983-04-05 1997-08-21 British Aerospace Verbindungsvorrichtung
FR2584456B1 (fr) * 1985-07-03 1987-10-02 Poudres & Explosifs Ste Nale Dispositif de fermeture temporaire d'un orifice interne d'un propulseur
EP0229457B1 (fr) * 1985-10-31 1991-03-13 British Aerospace Public Limited Company Fusée éclairante pour raquette
DE3718716C2 (de) * 1986-08-02 1988-06-30 Messerschmitt Boelkow Blohm Geschoss
US4803928A (en) * 1986-08-02 1989-02-14 Stefan Kramer Tandem charge projectile
FR2613824B1 (fr) * 1987-04-10 1993-05-28 Lacroix E Tous Artifices Roquette autopropulsee et dispositif pyrotechnique de lancement incorporant celle-ci
FR2657158B1 (fr) * 1990-01-16 1994-05-27 Thomson Brandt Armements Munition perforante pour cible a haute resistance mecanique.
ATE168768T1 (de) * 1990-01-16 1998-08-15 Tda Armements Sas Penetratormunition für ziele mit hohem mechanischem widerstand
IL115749A (en) * 1994-10-27 2000-02-29 Thomson Csf Missile launching and orientating system

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH196392A (fr) * 1936-12-31 1938-03-15 Sageb Societe Anonyme De Gesti Projectile muni d'une fusée percutante.
US2458475A (en) * 1943-04-02 1949-01-04 Charles C Lauritsen Rocket device
US2421522A (en) * 1944-08-23 1947-06-03 Winslow B Pope Rocket projector and projectile
US2724237A (en) * 1946-03-05 1955-11-22 Clarence N Hickman Rocket projectile having discrete flight initiating and sustaining chambers
FR1291041A (fr) * 1961-03-10 1962-04-20 Hotchkiss Brandt Dispositif éjectable d'obturation et d'allumage pour projectile autopropulsé et projectile en comportant application
FR1328459A (fr) * 1962-04-18 1963-05-31 Soc Tech De Rech Ind Roquette à propulseur largable
US3136872A (en) * 1962-07-23 1964-06-09 Lloyd J Banaszak Gas operated ignition switch for a multi-stage rocket propelled missile
FR1435514A (fr) * 1964-06-05 1966-04-15 British Aircraft Corp Ltd Dispositif de séparation entre un satellite et sa fusée porteuse
FR1513277A (fr) * 1966-07-27 1968-02-16 Hotchkiss Brandt Procédé pour l'envoi d'un engin dans l'espace et engin adapté pour la mise en oeuvre de ce procédé
US3438303A (en) * 1966-11-30 1969-04-15 Bombrini Parodi Delfino Spa System including a tubular launching tube and a rocket provided with an outer auxiliary launching charge
BE757634A (fr) * 1969-10-17 1971-04-01 Bofors Ab Dispositif d'allumage pour un projectile assiste d'une fusee
FR2260078A1 (en) * 1973-07-05 1975-08-29 Luchaire Sa Auxiliary charge for rocket launcher - has partition forming chamber ahead of launching member for extra acceleration

Also Published As

Publication number Publication date
DE2757806C2 (de) 1986-07-10
FR2376300B1 (fr) 1981-11-06
FR2376300A1 (fr) 1978-07-28
GB1543690A (en) 1979-04-04
SE7714509L (sv) 1978-06-29
US4250705A (en) 1981-02-17
SE421831B (sv) 1982-02-01
DE2757806A1 (de) 1978-07-13
IT1091528B (it) 1985-07-06

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Legal Events

Date Code Title Description
RE Patent lapsed

Owner name: SOC. NATIONALE DES POUDRES ET EXPLOSIFS

Effective date: 19961231

Owner name: LUCHAIRE S.A.

Effective date: 19961231