FR1197701A - Device suitable for steering rocket-propelled mobiles - Google Patents

Device suitable for steering rocket-propelled mobiles

Info

Publication number
FR1197701A
FR1197701A FR1197701DA FR1197701A FR 1197701 A FR1197701 A FR 1197701A FR 1197701D A FR1197701D A FR 1197701DA FR 1197701 A FR1197701 A FR 1197701A
Authority
FR
France
Prior art keywords
mobiles
propelled
device suitable
steering rocket
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
Other languages
French (fr)
Inventor
Bertin Marcel Kados Jean-Henri
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.)
Bertin Technologies SAS
Original Assignee
Bertin et Cie 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 Bertin et Cie SA filed Critical Bertin et Cie SA
Application granted granted Critical
Publication of FR1197701A publication Critical patent/FR1197701A/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
    • F02K9/82—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control by injection of a secondary fluid into the rocket exhaust gases

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR1197701D 1957-12-11 1957-12-11 Device suitable for steering rocket-propelled mobiles Expired FR1197701A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1197701T 1957-12-11

Publications (1)

Publication Number Publication Date
FR1197701A true FR1197701A (en) 1959-12-02

Family

ID=9669780

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1197701D Expired FR1197701A (en) 1957-12-11 1957-12-11 Device suitable for steering rocket-propelled mobiles

Country Status (1)

Country Link
FR (1) FR1197701A (en)

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3091924A (en) * 1960-12-15 1963-06-04 United Aircraft Corp Gaseous nozzle boundary
US3092963A (en) * 1960-12-15 1963-06-11 United Aircraft Corp Vector control system
US3101591A (en) * 1961-03-28 1963-08-27 Thompson Ramo Wooldridge Inc Vapor-gas injection thrust vector control system
US3116603A (en) * 1961-08-15 1964-01-07 United Aircraft Corp Combined nozzle cooling and thrust vectoring
US3132476A (en) * 1961-04-27 1964-05-12 Earl W Conrad Thrust vector control apparatus
US3132478A (en) * 1961-07-13 1964-05-12 Thompson Ramo Wooldridge Inc Solid propellant gas rotary valve
US3133413A (en) * 1960-09-12 1964-05-19 United Aircraft Corp Control and cooling of rocket motors
US3137126A (en) * 1961-01-11 1964-06-16 North American Aviation Inc Method and means for forming a gaseous passage
US3144752A (en) * 1961-10-02 1964-08-18 United Aircraft Corp Injection thrust vectoring
US3212259A (en) * 1962-11-19 1965-10-19 Kepler Charles Edward Tertiary flow injection thrust vectoring system
US3213611A (en) * 1962-04-23 1965-10-26 Bendix Corp Valve
US3228188A (en) * 1963-03-29 1966-01-11 Atlantic Res Corp Thrust-vector control system
US3239150A (en) * 1961-11-29 1966-03-08 Continental Aviat & Eng Corp Thrust vector control
US3255971A (en) * 1962-11-21 1966-06-14 Bendix Corp Jet thrust vector control apparatus

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3133413A (en) * 1960-09-12 1964-05-19 United Aircraft Corp Control and cooling of rocket motors
US3092963A (en) * 1960-12-15 1963-06-11 United Aircraft Corp Vector control system
US3091924A (en) * 1960-12-15 1963-06-04 United Aircraft Corp Gaseous nozzle boundary
US3137126A (en) * 1961-01-11 1964-06-16 North American Aviation Inc Method and means for forming a gaseous passage
US3101591A (en) * 1961-03-28 1963-08-27 Thompson Ramo Wooldridge Inc Vapor-gas injection thrust vector control system
US3132476A (en) * 1961-04-27 1964-05-12 Earl W Conrad Thrust vector control apparatus
US3132478A (en) * 1961-07-13 1964-05-12 Thompson Ramo Wooldridge Inc Solid propellant gas rotary valve
US3116603A (en) * 1961-08-15 1964-01-07 United Aircraft Corp Combined nozzle cooling and thrust vectoring
US3144752A (en) * 1961-10-02 1964-08-18 United Aircraft Corp Injection thrust vectoring
US3239150A (en) * 1961-11-29 1966-03-08 Continental Aviat & Eng Corp Thrust vector control
US3213611A (en) * 1962-04-23 1965-10-26 Bendix Corp Valve
US3212259A (en) * 1962-11-19 1965-10-19 Kepler Charles Edward Tertiary flow injection thrust vectoring system
US3255971A (en) * 1962-11-21 1966-06-14 Bendix Corp Jet thrust vector control apparatus
US3228188A (en) * 1963-03-29 1966-01-11 Atlantic Res Corp Thrust-vector control system

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