AU3333495A - Synthesised fuel-powered reaction rocket motor - Google Patents

Synthesised fuel-powered reaction rocket motor

Info

Publication number
AU3333495A
AU3333495A AU33334/95A AU3333495A AU3333495A AU 3333495 A AU3333495 A AU 3333495A AU 33334/95 A AU33334/95 A AU 33334/95A AU 3333495 A AU3333495 A AU 3333495A AU 3333495 A AU3333495 A AU 3333495A
Authority
AU
Australia
Prior art keywords
rocket motor
powered reaction
synthesised
fuel
synthesised fuel
Prior art date
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.)
Abandoned
Application number
AU33334/95A
Inventor
Igor Urban
Original Assignee
Igor Urban
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
Priority to SI9400154 priority Critical
Priority to SI9400154A priority patent/SI9400154A/en
Application filed by Igor Urban filed Critical Igor Urban
Priority to PCT/SI1995/000008 priority patent/WO1995026467A2/en
Publication of AU3333495A publication Critical patent/AU3333495A/en
Abandoned legal-status Critical Current

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
    • F02K9/42Rocket- engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/425Rocket- engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants propellants
    • 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
    • F02K9/42Rocket- engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/44Feeding propellants
    • 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
    • F02K9/42Rocket- engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/60Constructional parts; Details
    • F02K9/62Combustion or thrust chambers
    • F02K9/64Combustion or thrust chambers having cooling arrangements
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/20Heat transfer, e.g. cooling
    • F05D2260/205Cooling fluid recirculation, i.e. after cooling one or more components is the cooling fluid recovered and used elsewhere for other purposes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/20Heat transfer, e.g. cooling
    • F05D2260/232Heat transfer, e.g. cooling characterized by the cooling medium
AU33334/95A 1994-03-29 1995-03-28 Synthesised fuel-powered reaction rocket motor Abandoned AU3333495A (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
SI9400154 1994-03-29
SI9400154A SI9400154A (en) 1994-03-29 1994-03-29 Reaction rocket engine with synthetic fuel
PCT/SI1995/000008 WO1995026467A2 (en) 1994-03-29 1995-03-28 Bipropellant rocket motor

Publications (1)

Publication Number Publication Date
AU3333495A true AU3333495A (en) 1995-10-17

Family

ID=20431365

Family Applications (1)

Application Number Title Priority Date Filing Date
AU33334/95A Abandoned AU3333495A (en) 1994-03-29 1995-03-28 Synthesised fuel-powered reaction rocket motor

Country Status (3)

Country Link
AU (1) AU3333495A (en)
SI (1) SI9400154A (en)
WO (1) WO1995026467A2 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6052987A (en) * 1997-11-14 2000-04-25 Trw Inc. Non-propellant fluid cooled space craft rocket engine
DE102005030437B4 (en) 2005-06-30 2007-09-13 Deutsches Zentrum für Luft- und Raumfahrt e.V. Drive device based on gel-type fuel and method for fuel delivery
EP2103798A1 (en) 2008-03-20 2009-09-23 Aquafuel Research Limited Combustion method and apparatus

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2928240A (en) * 1953-01-27 1960-03-15 Thiokol Chemical Corp Control system for reaction motor ignitors
GB792909A (en) * 1953-06-19 1958-04-02 Havilland Engine Co Ltd Rocket motor cooling systems
US2981059A (en) * 1958-02-04 1961-04-25 Thompson Ramo Wooldridge Inc Dual thrust chamber rocket
US3140582A (en) * 1959-04-14 1964-07-14 Olin Mathieson Rocket propulsion method using boron and nitrogen compounds
GB2167401A (en) * 1984-09-25 1986-05-29 Kevin Maurice Buckley Injection nitration engine

Also Published As

Publication number Publication date
SI9400154A (en) 1995-12-31
WO1995026467A3 (en) 1995-11-09
WO1995026467A2 (en) 1995-10-05

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