FR1286239A - Perfectionnements apportés aux propulseurs pour fusées - Google Patents

Perfectionnements apportés aux propulseurs pour fusées

Info

Publication number
FR1286239A
FR1286239A FR858389A FR858389A FR1286239A FR 1286239 A FR1286239 A FR 1286239A FR 858389 A FR858389 A FR 858389A FR 858389 A FR858389 A FR 858389A FR 1286239 A FR1286239 A FR 1286239A
Authority
FR
France
Prior art keywords
rocket thrusters
thrusters
rocket
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
FR858389A
Other languages
English (en)
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 Technologies Corp
Original Assignee
United Aircraft Corp
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 United Aircraft Corp filed Critical United Aircraft Corp
Priority to FR858389A priority Critical patent/FR1286239A/fr
Application granted granted Critical
Publication of FR1286239A publication Critical patent/FR1286239A/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
    • F02K9/80—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
    • F02K9/84—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control using movable nozzles
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/60—Steering arrangements
    • F42B10/66—Steering by varying intensity or direction of thrust
    • F42B10/666—Steering by varying intensity or direction of thrust characterised by using a nozzle rotatable about an axis transverse to the axis of the projectile

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
FR858389A 1961-04-11 1961-04-11 Perfectionnements apportés aux propulseurs pour fusées Expired FR1286239A (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR858389A FR1286239A (fr) 1961-04-11 1961-04-11 Perfectionnements apportés aux propulseurs pour fusées

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR858389A FR1286239A (fr) 1961-04-11 1961-04-11 Perfectionnements apportés aux propulseurs pour fusées

Publications (1)

Publication Number Publication Date
FR1286239A true FR1286239A (fr) 1962-03-02

Family

ID=8752809

Family Applications (1)

Application Number Title Priority Date Filing Date
FR858389A Expired FR1286239A (fr) 1961-04-11 1961-04-11 Perfectionnements apportés aux propulseurs pour fusées

Country Status (1)

Country Link
FR (1) FR1286239A (fr)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1185417B (de) * 1962-03-20 1965-01-14 Snecma Dichtungs- und Lagerungsvorrichtung fuer eine Raketenduese
US4852827A (en) * 1987-03-14 1989-08-01 Messerschmitt-Bolkow-Blohm Gmbh Apparatus for controlling a projectile
FR3072732A1 (fr) * 2017-10-24 2019-04-26 Centre National D'etudes Spatiales Tuyere rotative, systeme de propulsion comprenant une telle tuyere et lanceur spatial comprenant un tel systeme de propulsion

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1185417B (de) * 1962-03-20 1965-01-14 Snecma Dichtungs- und Lagerungsvorrichtung fuer eine Raketenduese
US4852827A (en) * 1987-03-14 1989-08-01 Messerschmitt-Bolkow-Blohm Gmbh Apparatus for controlling a projectile
FR3072732A1 (fr) * 2017-10-24 2019-04-26 Centre National D'etudes Spatiales Tuyere rotative, systeme de propulsion comprenant une telle tuyere et lanceur spatial comprenant un tel systeme de propulsion

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