GB2196394B - Rocket propulsion system. - Google Patents

Rocket propulsion system.

Info

Publication number: GB2196394B
Authority: GB; United Kingdom
Prior art keywords: propulsion system; rocket propulsion; rocket; propulsion
Prior art date: 1986-10-14
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 - Lifetime

Application number

GB8724107A

Other versions

GB8724107D0 (en

GB2196394A (en

Inventor

George Albert Coffinberry

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.)

General Electric Co

Original Assignee

General Electric Co

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.)

1986-10-14

Filing date

1987-10-14

Publication date

1991-06-26

1987-10-14 Application filed by General Electric Co filed Critical General Electric Co

1987-11-18 Publication of GB8724107D0 publication Critical patent/GB8724107D0/en

1988-04-27 Publication of GB2196394A publication Critical patent/GB2196394A/en

1991-06-26 Application granted granted Critical

1991-06-26 Publication of GB2196394B publication Critical patent/GB2196394B/en

2007-10-14 Anticipated expiration legal-status Critical

Status Expired - Lifetime legal-status Critical Current

Classifications

- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
- F02K7/10—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
- F02K7/18—Composite ram-jet/rocket engines
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
- F02K7/10—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
- F02K7/14—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines with external combustion, e.g. scram-jet engines
- 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
- F02K9/08—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
- F02K9/32—Constructional parts; Details not otherwise provided for
- F02K9/34—Casings; Combustion chambers; Liners thereof
- 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
- 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
- F02K9/52—Injectors
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/40—Continuous combustion chambers using liquid or gaseous fuel characterised by the use of catalytic means

Landscapes

Engineering & Computer Science (AREA)
Chemical & Material Sciences (AREA)
Combustion & Propulsion (AREA)
Mechanical Engineering (AREA)
General Engineering & Computer Science (AREA)
Chemical Kinetics & Catalysis (AREA)
Filling Or Discharging Of Gas Storage Vessels (AREA)
Processing Of Solid Wastes (AREA)
Feeding Of Workpieces (AREA)
Vending Machines For Individual Products (AREA)

GB8724107A 1986-10-14 1987-10-14 Rocket propulsion system. Expired - Lifetime GB2196394B (en)

Applications Claiming Priority (1)

Application Number	Priority Date	Filing Date	Title
US91821786A	1986-10-14	1986-10-14

Publications (3)

Publication Number	Publication Date
GB8724107D0 GB8724107D0 (en)	1987-11-18
GB2196394A GB2196394A (en)	1988-04-27
GB2196394B true GB2196394B (en)	1991-06-26

Family

ID=25440002

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
GB8724107A Expired - Lifetime GB2196394B (en)	1986-10-14	1987-10-14	Rocket propulsion system.

Country Status (8)

Country	Link
JP (1)	JPS63120842A (en)
CN (1)	CN87106913A (en)
DE (1)	DE3734099A1 (en)
FR (1)	FR2605053A1 (en)
GB (1)	GB2196394B (en)
IT (1)	IT1225459B (en)
NO (1)	NO874263L (en)
SE (1)	SE464719B (en)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
DE3911655C1 (en) *	1989-04-10	1990-06-07	Messerschmitt-Boelkow-Blohm Gmbh, 8012 Ottobrunn, De	Cryogenic supersonic aircraft fuel tank - is surrounded by fuel pipe harness to permit heating or cooling
DE4437524C2 (en) *	1994-10-20	1997-04-24	Kunkel Klaus Dr Ing	Method for operating a missile propulsion system and missile propulsion
DE19927735B4 (en) *	1999-06-17	2005-10-06	Eads Space Transportation Gmbh	Thrust chamber arrangement for aerospace engines
RU2179256C2 (en) *	1999-06-21	2002-02-10	Открытое акционерное общество Самарский научно-технический комплекс им. Н.Д. Кузнецова	Liquid-propellant rocket engine gas generator
US7213392B2 (en) *	2003-06-10	2007-05-08	United Technologies Corporation	Rocket engine combustion chamber
RU2344310C2 (en) *	2005-12-02	2009-01-20	Федеральное государственное унитарное предприятие "Научно-исследовательский институт машиностроения" (ФГУП "НИИМаш")	Method for internal cooling of two-component liquid-propellant thruster and device for its realisation
DE102014107316A1 (en) *	2014-05-23	2015-11-26	Airbus Operations Gmbh	Tank system for the cryogenic storage of hydrogen and aircraft with a tank system for the cryogenic storage of hydrogen
DE102017106758A1 (en)	2017-03-15	2018-09-20	Deutsches Zentrum für Luft- und Raumfahrt e.V.	Thrust chamber device and method for operating a thrust chamber device
CN109162831A (en) *	2018-09-05	2019-01-08	北京航空航天大学	Solid-liquid power engine and the rocket for applying it
RU2752960C1 (en) *	2020-07-03	2021-08-11	Виктор Николаевич Исаков	Combustion chamber with catalytic coating for ramjet engine and method for applying a catalytic coating
DE102020123422A1 (en) *	2020-09-08	2022-03-31	Deutsches Zentrum für Luft- und Raumfahrt e.V.	Thrust chamber device and method for operating a thrust chamber device
CN112298501B (en) *	2020-10-20	2023-06-16	广东石油化工学院	Winged electric extrusion propulsion type intelligent underwater unmanned aircraft
CN112298502A (en) *	2020-10-20	2021-02-02	广东石油化工学院	Wingless electric extrusion spiral rotation forward type intelligent underwater unmanned vehicle
CN113357052B (en) *	2021-06-25	2022-07-19	中国科学院力学研究所	A method for controlling the uniform retreat of the combustion surface of the grain column of a solid-liquid engine
CN119844240A (en) *	2025-03-19	2025-04-18	中国空气动力研究与发展中心空天技术研究所	Gas-driven integrated support plate pulse injector and application method
CN119982251B (en) *	2025-04-15	2025-08-29	深圳驭龙航天科技有限公司	direct-drive liquid rocket engine

Citations (8)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
GB459924A (en) *	1935-02-09	1937-01-18	Eugen Saenger	Improvements in or relating to rocket engines
GB793300A (en) *	1953-06-19	1958-04-16	Havilland Engine Co Ltd	Rocket motors
GB800354A (en) *	1955-12-23	1958-08-27	Aerojet General Co	Combustion chamber for gas generation provided with cooling means and a system for operating the same
GB865942A (en) *	1958-10-10	1961-04-26	Gen Motors Corp	Improvements relating to exhaust ducts included in jet propulsion engines
GB970222A (en) *	1962-04-17	1964-09-16	Anders Folke Anden	Improvements in liquid fuel burning apparatus
GB1196489A (en) *	1966-11-29	1970-06-24	Lutz Tilo Kayser	Improvements in or relating to Rocket Engines
GB2006881A (en) *	1977-10-21	1979-05-10	Rolls Royce	Combustion apparatus for gas turbine engines
WO1981001186A1 (en) *	1979-10-25	1981-04-30	Dala Invest Ab	Method and device for obtaining microdrops

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
DE1085719B (en) *	1944-12-04	1960-07-21	Dr Eberhard Schneller	Rocket propulsion and training
US2526222A (en) *	1948-01-02	1950-10-17	Daniel And Florence Guggenheim	Cooling and feeding means for rocket type combustion chambers
BE490776A (en) *	1948-10-26
US2695496A (en) *	1952-03-05	1954-11-30	Daniel And Florence Guggenheim	Structure for feeding, intermingling, vaporizing, and igniting combustion liquids ina combustion chamber for rocket-type propulsion apparatus
US2749706A (en) *	1953-10-29	1956-06-12	Daniel And Florence Guggenheim	Mechanism for cooling a combustion chamber in propulsion apparatus and for feeding combustion liquids thereto
US3067594A (en) *	1959-05-11	1962-12-11	Catacycle Company	Cooling with endothermic chemical reactions
DE1626066C3 (en) *	1967-09-23	1974-06-12	Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen	Process for generating pressurized gas by catalytic decomposition of a liquid monergol and device for carrying out the process
US4535518A (en) *	1983-09-19	1985-08-20	Rockwell International Corporation	Method of forming small-diameter channel within an object

1987
- 1987-10-08 FR FR8713896A patent/FR2605053A1/en not_active Withdrawn
- 1987-10-09 DE DE19873734099 patent/DE3734099A1/en not_active Withdrawn
- 1987-10-09 IT IT8722207A patent/IT1225459B/en active
- 1987-10-13 CN CN198787106913A patent/CN87106913A/en active Pending
- 1987-10-13 SE SE8703970A patent/SE464719B/en not_active IP Right Cessation
- 1987-10-13 NO NO874263A patent/NO874263L/en unknown
- 1987-10-13 JP JP62256460A patent/JPS63120842A/en active Pending
- 1987-10-14 GB GB8724107A patent/GB2196394B/en not_active Expired - Lifetime

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
GB459924A (en) *	1935-02-09	1937-01-18	Eugen Saenger	Improvements in or relating to rocket engines
GB793300A (en) *	1953-06-19	1958-04-16	Havilland Engine Co Ltd	Rocket motors
GB800354A (en) *	1955-12-23	1958-08-27	Aerojet General Co	Combustion chamber for gas generation provided with cooling means and a system for operating the same
GB865942A (en) *	1958-10-10	1961-04-26	Gen Motors Corp	Improvements relating to exhaust ducts included in jet propulsion engines
GB970222A (en) *	1962-04-17	1964-09-16	Anders Folke Anden	Improvements in liquid fuel burning apparatus
GB1196489A (en) *	1966-11-29	1970-06-24	Lutz Tilo Kayser	Improvements in or relating to Rocket Engines
GB2006881A (en) *	1977-10-21	1979-05-10	Rolls Royce	Combustion apparatus for gas turbine engines
WO1981001186A1 (en) *	1979-10-25	1981-04-30	Dala Invest Ab	Method and device for obtaining microdrops

Also Published As

Publication number	Publication date
JPS63120842A (en)	1988-05-25
GB8724107D0 (en)	1987-11-18
CN87106913A (en)	1988-07-13
NO874263L (en)	1988-04-15
FR2605053A1 (en)	1988-04-15
NO874263D0 (en)	1987-10-13
SE464719B (en)	1991-06-03
IT8722207A0 (en)	1987-10-09
GB2196394A (en)	1988-04-27
DE3734099A1 (en)	1988-04-21
IT1225459B (en)	1990-11-14
SE8703970D0 (en)	1987-10-13
SE8703970L (en)	1988-04-15

Publication	Publication Date	Title
GB2196391B (en)	1991-06-26	Rocket propulsion system.
GB2196392B (en)	1991-06-26	Rocket propulsion system.
GB2208502B (en)	1991-10-02	Aircraft propulsion system.
EP0247388A3 (en)	1988-09-14	Rocket propulsion system having air-breathing possibilities
GB2227525B (en)	1993-10-13	Arcjet thruster
GB8708841D0 (en)	1987-05-20	Propulsion control
GB8902213D0 (en)	1989-03-22	Marine propulsion system
DE3787875D1 (en)	1993-11-25	Thermophotovoltaisches system.
EP0166178A3 (en)	1987-03-04	Propulsion slip-regulating system
GB8609228D0 (en)	1986-05-21	Thrusters
GB2196394B (en)	1991-06-26	Rocket propulsion system.
GB8610849D0 (en)	1986-08-20	Gas thruster
IL84671A0 (en)	1988-05-31	Aircraft propulsion system
GB2226088B (en)	1993-05-12	Aircraft propulsion system.
GB2196393B (en)	1991-07-17	Improvements relating to rocket casings.
EP0617348A3 (en)	1994-11-02	Aircraft propulsion control system.
GB8903836D0 (en)	1989-04-05	Propulsion system
GB8624460D0 (en)	1986-11-19	Sailing system
EP0266434A4 (en)	1989-11-07	Steering system.
GB8602497D0 (en)	1986-04-16	Rocket launcher
EP0303665A4 (en)	1989-06-13	Power boat construction system.
GB8828600D0 (en)	1989-01-11	Thrustless propulsion
GB8616571D0 (en)	1986-08-13	Vehicle propulsion system
GB8607550D0 (en)	1986-04-30	Multiple rudder systems
GB8622074D0 (en)	1986-10-22	Propulsion system

Legal Events

Date	Code	Title	Description
1993-06-09	PCNP	Patent ceased through non-payment of renewal fee	Effective date: 19921014