GB694371A - Control system for a rocket motor - Google Patents

Control system for a rocket motor

Info

Publication number
GB694371A
GB694371A GB22153/50A GB2215350A GB694371A GB 694371 A GB694371 A GB 694371A GB 22153/50 A GB22153/50 A GB 22153/50A GB 2215350 A GB2215350 A GB 2215350A GB 694371 A GB694371 A GB 694371A
Authority
GB
United Kingdom
Prior art keywords
valve
switch
pump
oxidizer
fuel
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
GB22153/50A
Other languages
English (en)
Inventor
Sidney Allen
Dennis Hurden
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
Priority to BE508931D priority Critical patent/BE508931A/xx
Application filed by Armstrong Siddeley Motors Ltd filed Critical Armstrong Siddeley Motors Ltd
Priority to GB22153/50A priority patent/GB694371A/en
Priority to US240216A priority patent/US2708342A/en
Priority to FR1049903D priority patent/FR1049903A/fr
Priority to DEA15039A priority patent/DE941102C/de
Priority to CH323427D priority patent/CH323427A/fr
Publication of GB694371A publication Critical patent/GB694371A/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
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/44—Feeding propellants
    • F02K9/56—Control

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Testing Of Engines (AREA)
  • Output Control And Ontrol Of Special Type Engine (AREA)
GB22153/50A 1950-09-08 1950-09-08 Control system for a rocket motor Expired GB694371A (en)

Priority Applications (6)

Application Number Priority Date Filing Date Title
BE508931D BE508931A (it) 1950-09-08
GB22153/50A GB694371A (en) 1950-09-08 1950-09-08 Control system for a rocket motor
US240216A US2708342A (en) 1950-09-08 1951-08-03 Mixed fuel control system for a rocket motor
FR1049903D FR1049903A (fr) 1950-09-08 1952-01-26 Dispositif de commande pour moteur-fusée
DEA15039A DE941102C (de) 1950-09-08 1952-01-29 Betaetigungs- und Steuereinrichtung fuer die Zufuhr von fluessigem Brennstoff und fluessigem Sauerstofftraeger zu einer Verbrennungs-einrichtung, insbesondere fuer Raketenantriebe
CH323427D CH323427A (fr) 1950-09-08 1952-01-30 Installation de propulsion à fusée

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB22153/50A GB694371A (en) 1950-09-08 1950-09-08 Control system for a rocket motor

Publications (1)

Publication Number Publication Date
GB694371A true GB694371A (en) 1953-07-22

Family

ID=10174781

Family Applications (1)

Application Number Title Priority Date Filing Date
GB22153/50A Expired GB694371A (en) 1950-09-08 1950-09-08 Control system for a rocket motor

Country Status (5)

Country Link
US (1) US2708342A (it)
BE (1) BE508931A (it)
CH (1) CH323427A (it)
FR (1) FR1049903A (it)
GB (1) GB694371A (it)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2850874A (en) * 1954-03-22 1958-09-09 Plessey Co Ltd Control and ignition system for liquid fuel combustion apparatus
US2829491A (en) * 1954-09-02 1958-04-08 Bendix Aviat Corp Two-stage liquid fuel rocket
US2982503A (en) * 1954-12-14 1961-05-02 English Electric Co Ltd Rocket motor attachments
US2946186A (en) * 1956-02-10 1960-07-26 Thompson Ramo Wooldridge Inc Balanced regulator valve
US2971332A (en) * 1956-11-13 1961-02-14 Bendix Corp Electrical timing control apparatus
US2976682A (en) * 1958-04-09 1961-03-28 United Aircraft Corp Pneumatic control system for fuel-air starter
US4899536A (en) * 1988-07-21 1990-02-13 Sundstrand Corporation Starting system for a turbine engine
FR2699602B1 (fr) * 1992-12-22 1995-03-10 Europ Propulsion Système de délestage de liquide, notamment pour ensembles propulsifs.
CN112879805B (zh) * 2021-01-19 2021-12-31 北京航空航天大学 自带增压系统的车载移动式过氧化氢供应系统
CN114837853B (zh) * 2022-05-20 2024-01-16 西北工业大学 固液混合发动机多次启动点火方法及装置
CN116296421A (zh) * 2022-12-30 2023-06-23 北京天兵科技有限公司 一种火箭氧箱动力系统试车增补压装置及方法

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2395113A (en) * 1940-04-01 1946-02-19 Daniel And Florence Guggenheim Mechanism for feeding combustion liquids to rocket apparatus
US2397657A (en) * 1941-06-23 1946-04-02 Daniel And Florence Guggenheim Control mechanism for rocket apparatus
US2479888A (en) * 1943-07-06 1949-08-23 Reaction Motors Inc Controlling system for reaction motors
US2469678A (en) * 1943-12-18 1949-05-10 Edwin T Wyman Combination steam and gas turbine
US2470564A (en) * 1944-11-15 1949-05-17 Reaction Motors Inc Reaction motor control system

Also Published As

Publication number Publication date
US2708342A (en) 1955-05-17
CH323427A (fr) 1957-07-31
BE508931A (it)
FR1049903A (fr) 1954-01-04

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