CH539200A - Raketentriebwerk - Google Patents

Raketentriebwerk

Info

Publication number
CH539200A
CH539200A CH775371A CH775371A CH539200A CH 539200 A CH539200 A CH 539200A CH 775371 A CH775371 A CH 775371A CH 775371 A CH775371 A CH 775371A CH 539200 A CH539200 A CH 539200A
Authority
CH
Switzerland
Prior art keywords
rocket engine
rocket
engine
Prior art date
Application number
CH775371A
Other languages
English (en)
Inventor
Suter Xaver
Original Assignee
Oerlikon Buehrle Ag
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 Oerlikon Buehrle Ag filed Critical Oerlikon Buehrle Ag
Priority to CH775371A priority Critical patent/CH539200A/de
Priority to DE2221162A priority patent/DE2221162C3/de
Priority to SE7206008A priority patent/SE379398B/xx
Priority to FR7216946A priority patent/FR2138691B1/fr
Priority to US00254083A priority patent/US3779012A/en
Priority to GB2305372A priority patent/GB1352479A/en
Priority to BE783806A priority patent/BE783806A/xx
Priority to IT24693/72A priority patent/IT955744B/it
Priority to IL39523A priority patent/IL39523A/xx
Publication of CH539200A publication Critical patent/CH539200A/de

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/08Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/32Constructional parts; Details not otherwise provided for
    • F02K9/34Casings; Combustion chambers; Liners thereof
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/08Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/10Shape or structure of solid propellant charges
    • F02K9/12Shape or structure of solid propellant charges made of two or more portions burning at different rates or having different characteristics
CH775371A 1971-05-27 1971-05-27 Raketentriebwerk CH539200A (de)

Priority Applications (9)

Application Number Priority Date Filing Date Title
CH775371A CH539200A (de) 1971-05-27 1971-05-27 Raketentriebwerk
DE2221162A DE2221162C3 (de) 1971-05-27 1972-04-28 Feststoff-Raketentriebwerk
SE7206008A SE379398B (de) 1971-05-27 1972-05-05
FR7216946A FR2138691B1 (de) 1971-05-27 1972-05-12
US00254083A US3779012A (en) 1971-05-27 1972-05-17 Rocket engine
GB2305372A GB1352479A (en) 1971-05-27 1972-05-17 Rocket engine
BE783806A BE783806A (fr) 1971-05-27 1972-05-23 Propulseur pour roquettes
IT24693/72A IT955744B (it) 1971-05-27 1972-05-23 Gruppo propulsore per razzi
IL39523A IL39523A (en) 1971-05-27 1972-05-24 Rocket engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH775371A CH539200A (de) 1971-05-27 1971-05-27 Raketentriebwerk

Publications (1)

Publication Number Publication Date
CH539200A true CH539200A (de) 1973-07-15

Family

ID=4329960

Family Applications (1)

Application Number Title Priority Date Filing Date
CH775371A CH539200A (de) 1971-05-27 1971-05-27 Raketentriebwerk

Country Status (9)

Country Link
US (1) US3779012A (de)
BE (1) BE783806A (de)
CH (1) CH539200A (de)
DE (1) DE2221162C3 (de)
FR (1) FR2138691B1 (de)
GB (1) GB1352479A (de)
IL (1) IL39523A (de)
IT (1) IT955744B (de)
SE (1) SE379398B (de)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5101731A (en) * 1990-11-30 1992-04-07 The United States Of America As Represented By The Secretary Of The Navy Propellant grain assembly for a gas generator
RU2490499C1 (ru) * 2012-04-09 2013-08-20 Открытое акционерное общество "Научно-исследовательский институт полимерных материалов" Заряд твердого ракетного топлива
US8975565B2 (en) * 2012-07-17 2015-03-10 Raytheon Company Integrated propulsion and attitude control system from a common pressure vessel for an interceptor

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2944389A (en) * 1944-11-20 1960-07-12 Clarence E Weinland Rotating rocket motor and method of making same
US3165889A (en) * 1958-11-24 1965-01-19 Richard B Kershner Jet control by rotatable offset nozzle
US3151449A (en) * 1961-08-25 1964-10-06 Curtiss Wright Corp Rocket nozzle cooling system
US3147591A (en) * 1961-12-28 1964-09-08 Gen Motors Corp Swiveling fluid jet exhaust nozzle construction
US3520139A (en) * 1964-06-11 1970-07-14 Curtiss Wright Corp Nozzle coolant supply system

Also Published As

Publication number Publication date
DE2221162B2 (de) 1974-01-31
DE2221162C3 (de) 1974-08-22
GB1352479A (en) 1974-05-08
IT955744B (it) 1973-09-29
DE2221162A1 (de) 1972-11-30
BE783806A (fr) 1972-09-18
SE379398B (de) 1975-10-06
FR2138691B1 (de) 1975-03-21
IL39523A (en) 1974-07-31
FR2138691A1 (de) 1973-01-05
US3779012A (en) 1973-12-18
IL39523A0 (en) 1972-10-29

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Legal Events

Date Code Title Description
PL Patent ceased