FR1003758A - Perfectionnements aux réacteurs utilisés pour la propulsion par réaction - Google Patents

Perfectionnements aux réacteurs utilisés pour la propulsion par réaction

Info

Publication number
FR1003758A
FR1003758A FR1003758DA FR1003758A FR 1003758 A FR1003758 A FR 1003758A FR 1003758D A FR1003758D A FR 1003758DA FR 1003758 A FR1003758 A FR 1003758A
Authority
FR
France
Prior art keywords
jet propulsion
reactors used
reactors
propulsion
jet
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
English (en)
Inventor
M Precoul
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.)
SOC TECH DE RECH IND
Technique de Recherches Industrielles et Mecaniques
Original Assignee
SOC TECH DE RECH IND
Technique de Recherches Industrielles et Mecaniques
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 SOC TECH DE RECH IND, Technique de Recherches Industrielles et Mecaniques filed Critical SOC TECH DE RECH IND
Application granted granted Critical
Publication of FR1003758A publication Critical patent/FR1003758A/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
    • F02K9/12—Shape or structure of solid propellant charges made of two or more portions burning at different rates or having different characteristics
    • 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
    • F02K9/28—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants having two or more propellant charges with the propulsion gases exhausting through a common nozzle
    • 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
    • F02K9/40—Cooling arrangements
    • 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
FR1003758D 1947-02-21 1947-02-21 Perfectionnements aux réacteurs utilisés pour la propulsion par réaction Expired FR1003758A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1003758T 1947-02-21

Publications (1)

Publication Number Publication Date
FR1003758A true FR1003758A (fr) 1952-03-21

Family

ID=9563310

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1003758D Expired FR1003758A (fr) 1947-02-21 1947-02-21 Perfectionnements aux réacteurs utilisés pour la propulsion par réaction

Country Status (1)

Country Link
FR (1) FR1003758A (fr)

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3056260A (en) * 1957-10-31 1962-10-02 Standard Oil Co Temperature rise retardation of surfaces exposed to heat
US3069845A (en) * 1958-03-14 1962-12-25 Mini Of Supply Liner for cooling rocket motors
US3093964A (en) * 1960-12-14 1963-06-18 United Aircraft Corp Two-stage rocket
US3094072A (en) * 1957-12-09 1963-06-18 Arthur R Parilla Aircraft, missiles, missile weapons systems, and space ships
US3113429A (en) * 1961-02-14 1963-12-10 Cievite Corp Steering and speed control for jet propelled vehicles
US3122883A (en) * 1959-11-20 1964-03-03 Thompson Ramo Wooldridge Inc Heat resistant wall structure for rocket motor nozzles and the like
US3129560A (en) * 1960-06-13 1964-04-21 Stanley P Prosen Convectively cooled rocket nozzle
US3137995A (en) * 1960-01-26 1964-06-23 Chemical Engineering Dept Ablation resistant reaction propulsion nozzle
US3210933A (en) * 1963-10-11 1965-10-12 John P Crews Nozzle
US3251554A (en) * 1962-01-29 1966-05-17 Aerojet General Co Rocket motor nozzle
US3251267A (en) * 1963-06-18 1966-05-17 Emerson Electric Co Spin rocket and launcher
US3385063A (en) * 1962-03-19 1968-05-28 Air Force Usa Multi-stage solid propellant motor
US3521452A (en) * 1961-02-01 1970-07-21 Exxon Research Engineering Co Rocket nozzle cooling
FR2631387A1 (fr) * 1988-05-10 1989-11-17 Poudres & Explosifs Ste Nale Propulseur sans tuyere de faible allongement
FR2648518A1 (fr) * 1989-06-15 1990-12-21 Poudres & Explosifs Ste Nale Propulseur comprenant un bloc de propergol muni d'un canal central de section variable

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3056260A (en) * 1957-10-31 1962-10-02 Standard Oil Co Temperature rise retardation of surfaces exposed to heat
US3094072A (en) * 1957-12-09 1963-06-18 Arthur R Parilla Aircraft, missiles, missile weapons systems, and space ships
US3069845A (en) * 1958-03-14 1962-12-25 Mini Of Supply Liner for cooling rocket motors
US3122883A (en) * 1959-11-20 1964-03-03 Thompson Ramo Wooldridge Inc Heat resistant wall structure for rocket motor nozzles and the like
US3137995A (en) * 1960-01-26 1964-06-23 Chemical Engineering Dept Ablation resistant reaction propulsion nozzle
US3129560A (en) * 1960-06-13 1964-04-21 Stanley P Prosen Convectively cooled rocket nozzle
US3093964A (en) * 1960-12-14 1963-06-18 United Aircraft Corp Two-stage rocket
US3521452A (en) * 1961-02-01 1970-07-21 Exxon Research Engineering Co Rocket nozzle cooling
US3113429A (en) * 1961-02-14 1963-12-10 Cievite Corp Steering and speed control for jet propelled vehicles
US3251554A (en) * 1962-01-29 1966-05-17 Aerojet General Co Rocket motor nozzle
US3385063A (en) * 1962-03-19 1968-05-28 Air Force Usa Multi-stage solid propellant motor
US3251267A (en) * 1963-06-18 1966-05-17 Emerson Electric Co Spin rocket and launcher
US3210933A (en) * 1963-10-11 1965-10-12 John P Crews Nozzle
FR2631387A1 (fr) * 1988-05-10 1989-11-17 Poudres & Explosifs Ste Nale Propulseur sans tuyere de faible allongement
FR2648518A1 (fr) * 1989-06-15 1990-12-21 Poudres & Explosifs Ste Nale Propulseur comprenant un bloc de propergol muni d'un canal central de section variable

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