FR1178470A - Advanced nozzle for projectile thruster or other device - Google Patents

Advanced nozzle for projectile thruster or other device

Info

Publication number
FR1178470A
FR1178470A FR1178470DA FR1178470A FR 1178470 A FR1178470 A FR 1178470A FR 1178470D A FR1178470D A FR 1178470DA FR 1178470 A FR1178470 A FR 1178470A
Authority
FR
France
Prior art keywords
thruster
projectile
advanced nozzle
advanced
nozzle
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.)
Expired
Application number
Other languages
French (fr)
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.)
Hotchkiss Brandt SA
Original Assignee
Hotchkiss Brandt SA
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 Hotchkiss Brandt SA filed Critical Hotchkiss Brandt SA
Application granted granted Critical
Publication of FR1178470A publication Critical patent/FR1178470A/en
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
    • F02K9/80—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
    • F02K9/86—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control using nozzle throats of adjustable cross- section

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR1178470D 1957-04-19 1957-04-19 Advanced nozzle for projectile thruster or other device Expired FR1178470A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1178470T 1957-04-19

Publications (1)

Publication Number Publication Date
FR1178470A true FR1178470A (en) 1959-05-11

Family

ID=9660722

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1178470D Expired FR1178470A (en) 1957-04-19 1957-04-19 Advanced nozzle for projectile thruster or other device

Country Status (1)

Country Link
FR (1) FR1178470A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3760589A (en) * 1969-03-24 1973-09-25 Thiokol Chemical Corp Throttling mechanism for controlling the thrust level of a solid propellant rocket motor
DE1453854C1 (en) * 1964-04-13 1984-05-24 Philco-Ford Corp., Philadelphia, Pa. Remote-controlled missile
EP0234633A2 (en) * 1986-02-18 1987-09-02 Microtecnica S.p.A. Energetic stabilizing device for a generator of hot gases

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1453854C1 (en) * 1964-04-13 1984-05-24 Philco-Ford Corp., Philadelphia, Pa. Remote-controlled missile
US3760589A (en) * 1969-03-24 1973-09-25 Thiokol Chemical Corp Throttling mechanism for controlling the thrust level of a solid propellant rocket motor
EP0234633A2 (en) * 1986-02-18 1987-09-02 Microtecnica S.p.A. Energetic stabilizing device for a generator of hot gases
EP0234633A3 (en) * 1986-02-18 1988-08-31 Microtecnica S.P.A. Energetic stabilizing device for a generator of hot gases

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