IT1088833B - HEAT EXCHANGER, ESPECIALLY REGENERATIVE COOLING CHAMBER, WITH SPRAYER, FOR PROPULSORS FOR LIQUID PROPELLENT ROCKETS - Google Patents

HEAT EXCHANGER, ESPECIALLY REGENERATIVE COOLING CHAMBER, WITH SPRAYER, FOR PROPULSORS FOR LIQUID PROPELLENT ROCKETS

Info

Publication number
IT1088833B
IT1088833B IT3082677A IT3082677A IT1088833B IT 1088833 B IT1088833 B IT 1088833B IT 3082677 A IT3082677 A IT 3082677A IT 3082677 A IT3082677 A IT 3082677A IT 1088833 B IT1088833 B IT 1088833B
Authority
IT
Italy
Prior art keywords
propulsors
rockets
sprayer
heat exchanger
cooling chamber
Prior art date
Application number
IT3082677A
Other languages
Italian (it)
Original Assignee
Messerschmitt Boelkow Blohm
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 Messerschmitt Boelkow Blohm filed Critical Messerschmitt Boelkow Blohm
Application granted granted Critical
Publication of IT1088833B publication Critical patent/IT1088833B/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
    • F02K9/62—Combustion or thrust chambers
    • F02K9/64—Combustion or thrust chambers having cooling arrangements
IT3082677A 1976-12-18 1977-12-16 HEAT EXCHANGER, ESPECIALLY REGENERATIVE COOLING CHAMBER, WITH SPRAYER, FOR PROPULSORS FOR LIQUID PROPELLENT ROCKETS IT1088833B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19762657497 DE2657497A1 (en) 1976-12-18 1976-12-18 HEAT EXCHANGER, IN PARTICULAR REGENERATIVELY COOLED COMBUSTION CHAMBER WITH THROTTLE NOZZLE FOR LIQUID ROCKET ENGINES

Publications (1)

Publication Number Publication Date
IT1088833B true IT1088833B (en) 1985-06-10

Family

ID=5995893

Family Applications (1)

Application Number Title Priority Date Filing Date
IT3082677A IT1088833B (en) 1976-12-18 1977-12-16 HEAT EXCHANGER, ESPECIALLY REGENERATIVE COOLING CHAMBER, WITH SPRAYER, FOR PROPULSORS FOR LIQUID PROPELLENT ROCKETS

Country Status (3)

Country Link
DE (1) DE2657497A1 (en)
FR (1) FR2374520A1 (en)
IT (1) IT1088833B (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4015204C1 (en) * 1990-05-11 1991-10-17 Mtu Muenchen Gmbh
DE19804232C2 (en) * 1998-02-04 2000-06-29 Daimler Chrysler Ag Combustion chamber for high-performance engines and nozzles
WO2008076007A1 (en) * 2006-12-19 2008-06-26 Volvo Aero Corporation A method of manufacturing a wall structure and a machining tool

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3131535A (en) * 1960-04-07 1964-05-05 Pneumo Dynamics Corp Rocket nozzle
FR2012723A1 (en) * 1968-07-11 1970-03-20 Messerschmitt Boelkow Blohm
DE1751938B1 (en) * 1968-08-21 1970-12-03 Messerschmitt Boelkow Blohm Process for the production of the cooling ducts for rocket combustion chambers with convergent-divergent thrust nozzle
US3692637A (en) * 1969-11-24 1972-09-19 Carl Helmut Dederra Method of fabricating a hollow structure having cooling channels

Also Published As

Publication number Publication date
FR2374520A1 (en) 1978-07-13
DE2657497A1 (en) 1978-06-22

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