US2563022A
(en)
*
|
1944-02-12 |
1951-08-07 |
Daniel And Florence Guggenheim |
Fuel feeding mechanism for detonating combustion apparatus
|
US2520751A
(en)
*
|
1944-02-19 |
1950-08-29 |
Aerojet Engineering Corp |
Reaction motor with fluid cooling means
|
US2433932A
(en)
*
|
1944-03-11 |
1948-01-06 |
Aerojet Engineering Corp |
Fuel combustion
|
US2433943A
(en)
*
|
1944-03-11 |
1948-01-06 |
Aerojet Engineering Corp |
Operation of jet propulsion motors with nitroparaffin
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US3048007A
(en)
*
|
1944-03-31 |
1962-08-07 |
Aerojet General Co |
Decomposition of nitro-paraffins in jet propulsion motor operation
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US2645079A
(en)
*
|
1944-06-06 |
1953-07-14 |
Union Oil Co |
Method of operating jet propulsion motors
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US2447696A
(en)
*
|
1944-12-13 |
1948-08-24 |
Fairey Aviat Co Ltd |
Combustion gas and steam turbine arrangement
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US2445856A
(en)
*
|
1945-05-26 |
1948-07-27 |
Aerojet Engineering Corp |
Rotary reaction motor
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US2586025A
(en)
*
|
1946-01-05 |
1952-02-19 |
Homer C Godfrey |
Jet reaction engine of the turbine type
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US2633700A
(en)
*
|
1946-04-12 |
1953-04-07 |
Daniel And Florence Guggenheim |
Combustion chamber for propulsion apparatus and having multiple discharge nozzles
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US2591422A
(en)
*
|
1946-06-28 |
1952-04-01 |
Esther C Goddard |
Liquid fuel and oxidizer jacketed combustion chamber with axial conical fuel spreader
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US2591421A
(en)
*
|
1946-06-28 |
1952-04-01 |
Esther C Goddard |
Combustion chamber jacket with alternate cooling passages of fuel and oxidizer
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US2698513A
(en)
*
|
1947-12-29 |
1955-01-04 |
Phillips Petroleum Co |
Paraffin hydrocarbon fuel for and method of operating pulse-jet engines
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US2612746A
(en)
*
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1948-03-04 |
1952-10-07 |
Daniel And Florence Guggenheim |
Nozzle structure for effecting striated flow of combustion gases
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US2636342A
(en)
*
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1949-01-04 |
1953-04-28 |
Phillips Petroleum Co |
Method for increasing the thrust of jet engines by the use of rapidly decomposable nitrogen compounds
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US2698511A
(en)
*
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1949-03-21 |
1955-01-04 |
Phillips Petroleum Co |
Method of operating turbojet engines
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US3190070A
(en)
*
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1950-04-05 |
1965-06-22 |
Thiokol Chemical Corp |
Reaction motor construction
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US2991617A
(en)
*
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1950-12-01 |
1961-07-11 |
Gen Electric |
Jet motor combustion chamber
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GB759901A
(en)
*
|
1951-12-06 |
1956-10-24 |
Armstrong Siddeley Motors Ltd |
Combustion chambers
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GB794660A
(en)
*
|
1954-08-30 |
1958-05-07 |
Havilland Engine Co Ltd |
Heat exchangers
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US2937698A
(en)
*
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1954-11-10 |
1960-05-24 |
Chrysler Corp |
Pressure tank
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US2951336A
(en)
*
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1956-08-08 |
1960-09-06 |
Heinz E Mueller |
Chamber wall casting process and assembly
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US3057148A
(en)
*
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1956-10-01 |
1962-10-09 |
Aerojet General Co |
Means to improve adherence of lining materials to the inner surface of combustion chambers of rocket motors
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GB851448A
(en)
*
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1957-06-21 |
1960-10-19 |
Armstrong Siddeley Motors Ltd |
Improvements in and relating to combustion chambers
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US2977754A
(en)
*
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1958-01-29 |
1961-04-04 |
Thiokol Chemical Corp |
Rocket chamber with multi-pass axial flow coolant passageways
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GB853133A
(en)
*
|
1958-02-13 |
1960-11-02 |
Napier & Son Ltd |
Combustion chamber construction
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US3093963A
(en)
*
|
1959-07-17 |
1963-06-18 |
North American Aviation Inc |
Manifolded exhaust duct
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US3016695A
(en)
*
|
1960-05-31 |
1962-01-16 |
Thiokol Chemical Corp |
Reaction motor thrust chamber
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US3134224A
(en)
*
|
1961-05-26 |
1964-05-26 |
United Aircraft Corp |
Gas bleed from rocket chamber
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US3229359A
(en)
*
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1962-07-05 |
1966-01-18 |
Bruce E Kramer |
Method of forming a refractory metal rocket nozzle
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DE1240702B
(de)
*
|
1963-09-18 |
1967-05-18 |
Nsu Motorenwerke Ag |
Fluessigkeitsgekuehlte Gehaeuse fuer Brennkraftmaschinen und Kompressoren
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DE1264160B
(de)
*
|
1966-12-15 |
1968-03-21 |
Boelkow Gmbh |
Fluessigkeitsgekuehlte Bauteile, wie Raketenbrennkammern, und Verfahren zu deren Herstellung
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DE1751180A1
(de)
*
|
1968-04-18 |
1971-04-29 |
Messerschmitt Boelkow Blohm |
Ausbildung und Anordnung eines Zulaufringes oder Ablaufsammelringes fuer Schubduesen oder Brennkammern von Raketentriebwerken,insbesondere Fluessigkeitsraketentriebwerken
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FR2012723A1
(fr)
*
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1968-07-11 |
1970-03-20 |
Messerschmitt Boelkow Blohm |
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US4781019A
(en)
*
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1983-04-04 |
1988-11-01 |
Rockwell International Corporation |
Keel-rib coolant channels for rocket combustors
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US4840025A
(en)
*
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1986-10-14 |
1989-06-20 |
General Electric Company |
Multiple-propellant air vehicle and propulsion system
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US4841723A
(en)
*
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1986-10-14 |
1989-06-27 |
General Electric Company |
Multiple-propellant air vehicle and propulsion system
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US4811556A
(en)
*
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1986-10-14 |
1989-03-14 |
General Electric Company |
Multiple-propellant air vehicle and propulsion system
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US4817890A
(en)
*
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1986-10-14 |
1989-04-04 |
General Electric Company |
Multiple-propellant air vehicle and propulsion system
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US4835959A
(en)
*
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1986-10-14 |
1989-06-06 |
General Electric Company |
Multiple-propellant air vehicle and propulsion system
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FR2605053A1
(fr)
*
|
1986-10-14 |
1988-04-15 |
Gen Electric |
Aeronef a combustibles multiples, et son systeme de propulsion
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FR2656378B1
(fr)
*
|
1989-12-27 |
1992-04-30 |
Europ Propulsion |
Paroi refroidie pour chambre de combustion ou tuyere de moteur-fusee, moteur aerobie ou moteur combine.
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DE4115403A1
(de)
*
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1991-05-10 |
1992-11-12 |
Mtu Muenchen Gmbh |
Duesenwand
|
FR2736683B1
(fr)
*
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1995-07-11 |
1997-10-03 |
Europ Propulsion |
Mat d'injection a refroidissement ameliore
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FR2915528B1
(fr)
*
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2007-04-25 |
2012-07-06 |
Astrium Sas |
Procede et dispositif pour alimenter un moteur de propulsion spatiale en ergols cryogeniques liquides.
|