CH342416A - Method of operating a rocket propulsion installation and installation for implementing this method - Google Patents

Method of operating a rocket propulsion installation and installation for implementing this method

Info

Publication number
CH342416A
CH342416A CH342416DA CH342416A CH 342416 A CH342416 A CH 342416A CH 342416D A CH342416D A CH 342416DA CH 342416 A CH342416 A CH 342416A
Authority
CH
Switzerland
Prior art keywords
installation
implementing
operating
rocket propulsion
rocket
Prior art date
Application number
Other languages
French (fr)
Inventor
Bernard Halford Frank
Valentine Cleaver Arthur
Lawrence Lofts Denis
Original Assignee
Havilland Engine Company Limit
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 Havilland Engine Company Limit filed Critical Havilland Engine Company Limit
Publication of CH342416A publication Critical patent/CH342416A/en

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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Hydrogen, Water And Hydrids (AREA)
CH342416D 1959-11-15 1956-07-17 Method of operating a rocket propulsion installation and installation for implementing this method CH342416A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH342416X 1959-11-15

Publications (1)

Publication Number Publication Date
CH342416A true CH342416A (en) 1959-11-15

Family

ID=4506147

Family Applications (1)

Application Number Title Priority Date Filing Date
CH342416D CH342416A (en) 1959-11-15 1956-07-17 Method of operating a rocket propulsion installation and installation for implementing this method

Country Status (3)

Country Link
CH (1) CH342416A (en)
FR (1) FR1154975A (en)
GB (1) GB771896A (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1088291B (en) * 1953-06-19 1960-09-01 Havilland Engine Co Ltd De Rocket propulsion
US3091921A (en) * 1957-06-24 1963-06-04 Thiokol Chemical Corp Turborocket powerplant including turbine bypassing means for a portion of the propellant
US3091520A (en) * 1958-12-19 1963-05-28 North American Aviation Inc Radial outflow catalytic pack
DE1164753B (en) * 1959-12-12 1964-03-05 Boelkow Entwicklungen Kg Rocket engine for liquid fuels
US3453828A (en) * 1966-03-01 1969-07-08 Plessey Co Ltd Rocket propulsion unit for operation by liquid monofuel
US3581504A (en) * 1968-08-28 1971-06-01 Aerojet General Co Monopropellant turbo gas generator

Also Published As

Publication number Publication date
GB771896A (en) 1957-04-03
FR1154975A (en) 1958-04-18

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