IT8722207A0 - MULTIPLE PROPELLANT AIR VEHICLE AND PROPULSION SYSTEM - Google Patents
MULTIPLE PROPELLANT AIR VEHICLE AND PROPULSION SYSTEMInfo
- Publication number
- IT8722207A0 IT8722207A0 IT8722207A IT2220787A IT8722207A0 IT 8722207 A0 IT8722207 A0 IT 8722207A0 IT 8722207 A IT8722207 A IT 8722207A IT 2220787 A IT2220787 A IT 2220787A IT 8722207 A0 IT8722207 A0 IT 8722207A0
- Authority
- IT
- Italy
- Prior art keywords
- propulsion system
- air vehicle
- propellant air
- multiple propellant
- vehicle
- Prior art date
Links
- 239000003380 propellant Substances 0.000 title 1
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
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US91821786A | 1986-10-14 | 1986-10-14 |
Publications (2)
Publication Number | Publication Date |
---|---|
IT8722207A0 true IT8722207A0 (en) | 1987-10-09 |
IT1225459B IT1225459B (en) | 1990-11-14 |
Family
ID=25440002
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IT8722207A IT1225459B (en) | 1986-10-14 | 1987-10-09 | MULTI-PURPOSE AIRCRAFT VEHICLE AND 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 (12)
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 |
US7213392B2 (en) | 2003-06-10 | 2007-05-08 | United Technologies Corporation | Rocket engine combustion chamber |
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 |
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 |
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 |
CN113357052B (en) * | 2021-06-25 | 2022-07-19 | 中国科学院力学研究所 | Method for controlling uniform retreating of combustion surface of explosive column of solid-liquid engine |
Family Cites Families (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE716175C (en) * | 1935-02-09 | 1942-01-14 | Eugen Saenger Dr Ing | Rocket engine |
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 |
GB793300A (en) * | 1953-06-19 | 1958-04-16 | Havilland Engine Co Ltd | Rocket motors |
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 |
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 |
US3067594A (en) * | 1959-05-11 | 1962-12-11 | Catacycle Company | Cooling with endothermic chemical reactions |
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 |
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 |
US4271675A (en) * | 1977-10-21 | 1981-06-09 | Rolls-Royce Limited | Combustion apparatus for gas turbine engines |
CA1159356A (en) * | 1979-10-25 | 1983-12-27 | Kurt Skoog | Method and device for producing microdroplets of fluid |
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 JP JP62256460A patent/JPS63120842A/en active Pending
- 1987-10-13 NO NO874263A patent/NO874263L/en unknown
- 1987-10-13 SE SE8703970A patent/SE464719B/en not_active IP Right Cessation
- 1987-10-13 CN CN198787106913A patent/CN87106913A/en active Pending
- 1987-10-14 GB GB8724107A patent/GB2196394B/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
DE3734099A1 (en) | 1988-04-21 |
SE464719B (en) | 1991-06-03 |
GB2196394A (en) | 1988-04-27 |
GB2196394B (en) | 1991-06-26 |
NO874263D0 (en) | 1987-10-13 |
IT1225459B (en) | 1990-11-14 |
GB8724107D0 (en) | 1987-11-18 |
CN87106913A (en) | 1988-07-13 |
FR2605053A1 (en) | 1988-04-15 |
NO874263L (en) | 1988-04-15 |
SE8703970L (en) | 1988-04-15 |
JPS63120842A (en) | 1988-05-25 |
SE8703970D0 (en) | 1987-10-13 |
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