WO1995026467A3 - Bipropellant rocket motor - Google Patents

Bipropellant rocket motor Download PDF

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Publication number
WO1995026467A3
WO1995026467A3 PCT/SI1995/000008 SI9500008W WO9526467A3 WO 1995026467 A3 WO1995026467 A3 WO 1995026467A3 SI 9500008 W SI9500008 W SI 9500008W WO 9526467 A3 WO9526467 A3 WO 9526467A3
Authority
WO
WIPO (PCT)
Prior art keywords
synthesised
rocket motor
fuel
powered
bipropellant rocket
Prior art date
Application number
PCT/SI1995/000008
Other languages
French (fr)
Other versions
WO1995026467A2 (en
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
Application filed by Igor Urban filed Critical Igor Urban
Priority to AU33334/95A priority Critical patent/AU3333495A/en
Priority to EP95912545A priority patent/EP0832349A2/en
Publication of WO1995026467A2 publication Critical patent/WO1995026467A2/en
Publication of WO1995026467A3 publication Critical patent/WO1995026467A3/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
    • F02K9/425—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
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/20—Heat transfer, e.g. cooling
    • F05D2260/205—Cooling fluid recirculation, i.e. after cooling one or more components is the cooling fluid recovered and used elsewhere for other purposes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/20—Heat transfer, e.g. cooling
    • F05D2260/232—Heat transfer, e.g. cooling characterized by the cooling medium

Abstract

The invention is a synthesised fuel-powered reaction rocket motor, powered by fuels based on labile compounds which can be used as fuel only if they have previously been synthesised or processed. The synthesised fuel-powered reaction rocket motor has two synthesised compounds stored in separate tanks (1, 2), which are combined in the antechamber and which react in the combustion chamber (4). The resulting gases give the required thrust.
PCT/SI1995/000008 1994-03-29 1995-03-28 Bipropellant rocket motor WO1995026467A2 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
AU33334/95A AU3333495A (en) 1994-03-29 1995-03-28 Synthesised fuel-powered reaction rocket motor
EP95912545A EP0832349A2 (en) 1994-03-29 1995-03-28 Synthesised fuel-powered reaction rocket motor

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
SIP-9400154 1994-03-29
SI9400154A SI9400154A (en) 1994-03-29 1994-03-29 Reaction rocket engine with synthetic fuel

Publications (2)

Publication Number Publication Date
WO1995026467A2 WO1995026467A2 (en) 1995-10-05
WO1995026467A3 true WO1995026467A3 (en) 1995-11-09

Family

ID=20431365

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/SI1995/000008 WO1995026467A2 (en) 1994-03-29 1995-03-28 Bipropellant 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

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB792909A (en) * 1953-06-19 1958-04-02 Havilland Engine Co Ltd Rocket motor cooling systems
US2928240A (en) * 1953-01-27 1960-03-15 Thiokol Chemical Corp Control system for reaction motor ignitors
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

Patent Citations (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
AU3333495A (en) 1995-10-17
WO1995026467A2 (en) 1995-10-05
SI9400154A (en) 1995-12-31

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