FR1203995A - Moteur-fusée perfectionné - Google Patents

Moteur-fusée perfectionné

Info

Publication number
FR1203995A
FR1203995A FR1203995DA FR1203995A FR 1203995 A FR1203995 A FR 1203995A FR 1203995D A FR1203995D A FR 1203995DA FR 1203995 A FR1203995 A FR 1203995A
Authority
FR
France
Prior art keywords
rocket engine
advanced
advanced rocket
engine
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
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.)
Armstrong Siddeley Motors Ltd
Original Assignee
Armstrong Siddeley Motors Ltd
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 Armstrong Siddeley Motors Ltd filed Critical Armstrong Siddeley Motors Ltd
Application granted granted Critical
Publication of FR1203995A publication Critical patent/FR1203995A/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
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/60—Constructional parts; Details not otherwise provided for
    • F02K9/68—Decomposition chambers
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49346—Rocket or jet device making

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
FR1203995D 1956-07-05 1958-10-01 Moteur-fusée perfectionné Expired FR1203995A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB20824/56A GB809844A (en) 1956-07-05 1956-07-05 Improvements in and relating to rocket motors

Publications (1)

Publication Number Publication Date
FR1203995A true FR1203995A (fr) 1960-01-22

Family

ID=10152324

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1203995D Expired FR1203995A (fr) 1956-07-05 1958-10-01 Moteur-fusée perfectionné

Country Status (4)

Country Link
US (1) US2972227A (fr)
BE (1) BE571939A (fr)
FR (1) FR1203995A (fr)
GB (1) GB809844A (fr)

Families Citing this family (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3069850A (en) * 1959-05-18 1962-12-25 United Aircraft Corp Rocket nozzle with directional control
US3086358A (en) * 1959-05-25 1963-04-23 United Aircraft Corp Rocket nozzle construction
US3136036A (en) * 1959-05-29 1964-06-09 Dobell Curzon Method of making reinforced rocket nozzle
US3004386A (en) * 1959-06-23 1961-10-17 United Aircraft Corp Rocket nozzle tube construction
US3062566A (en) * 1959-06-25 1962-11-06 United Aircraft Corp Manifold attachment to tubular wall
US3135703A (en) * 1959-09-21 1964-06-02 Bell Aerospace Corp Thrust chamber catalyst structure
US2967393A (en) * 1959-12-03 1961-01-10 Braun Wernher Von Rocket-propelled missile
US3008672A (en) * 1960-10-04 1961-11-14 Bell Aerospace Corp Altitude responsive aircraft jet control
US3150485A (en) * 1961-11-24 1964-09-29 Frederick R Hickerson Variable thrust rocket engine
US3154920A (en) * 1961-11-30 1964-11-03 Gen Electric Catalytic igniter
US3120738A (en) * 1962-03-03 1964-02-11 James E Webb Ignition system for monopropellant combustion devices
US3173251A (en) * 1962-03-16 1965-03-16 Jr Harrison Allen Apparatus for igniting solid propellants
US3203172A (en) * 1962-06-27 1965-08-31 Rocket Research Corp Method of propulsion utilizing hybrid reaction engine with porous fuel grain
US3289943A (en) * 1962-08-17 1966-12-06 Westinghouse Electric Corp Thermal barrier for thrust vehicle nozzle
US3156094A (en) * 1962-11-21 1964-11-10 Gen Electric Catalytic ignition means for a jet engine thrust augmentation system
US3662547A (en) * 1970-03-16 1972-05-16 Nasa Coaxial injector for reaction motors
US3742701A (en) * 1971-06-16 1973-07-03 Us Navy Propellant injector assembly
US3903693A (en) * 1973-03-26 1975-09-09 Anthony Fox Rocket motor housing
JPS51145504A (en) * 1975-05-28 1976-12-14 Nissan Motor Co Ltd A reformer
CH612472A5 (fr) * 1976-03-05 1979-07-31 Sulzer Ag
CH613018A5 (fr) * 1976-04-07 1979-08-31 Sulzer Ag
US4352782A (en) * 1981-02-20 1982-10-05 Rocket Research Company Catalytic gas generator
JP6017453B2 (ja) * 2011-01-20 2016-11-02 キャスケイド デザインズ インコーポレイテッド 燃料および酸化剤を同時に計量するための燃料および酸化剤の複合型計量ジェット、システムおよび方法
US11603940B2 (en) * 2018-04-12 2023-03-14 Woodward, Inc. Damped check valve having multi-pressure operation
CN114017208B (zh) * 2021-12-09 2023-05-09 北京航空航天大学 固液火箭发动机催化床及其冷却和预热系统、方法
CN114876668B (zh) * 2022-03-21 2024-06-21 西安航天动力研究所 一种过氧化氢发动机及其控制方法

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2706887A (en) * 1946-01-23 1955-04-26 Harlow B Grow Liquid propellant rocket motor
US2555081A (en) * 1946-03-26 1951-05-29 Daniel And Florence Guggenheim Means for supplying liquids to an annular rotating combustion chamber
US2591880A (en) * 1948-01-10 1952-04-08 Lockheed Aircraft Corp Liquid and vapor control valve
US2763126A (en) * 1949-07-14 1956-09-18 Havilland Engine Co Ltd Fuel feeding and ignition means for rocket motors with non-self-igniting propellants
GB680717A (en) * 1949-07-14 1952-10-08 Havilland Engine Co Ltd Improvements relating to rocket motors
US2605609A (en) * 1950-09-14 1952-08-05 Gen Electric Motive mechanism utilizing catalytically decomposable material
GB727720A (en) * 1951-06-27 1955-04-06 Mini Of Supply Improvements in or relating to power units
US2791883A (en) * 1951-10-25 1957-05-14 Gen Electric Propellant system
GB794660A (en) * 1954-08-30 1958-05-07 Havilland Engine Co Ltd Heat exchangers
US2906091A (en) * 1957-11-27 1959-09-29 Kretschmer Willi Propellant systems for reaction motors

Also Published As

Publication number Publication date
GB809844A (en) 1959-03-04
BE571939A (fr) 1958-10-31
US2972227A (en) 1961-02-21

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