GB1534601A - Electrothermal gas thrusters - Google Patents

Electrothermal gas thrusters

Info

Publication number
GB1534601A
GB1534601A GB3085476A GB3085476A GB1534601A GB 1534601 A GB1534601 A GB 1534601A GB 3085476 A GB3085476 A GB 3085476A GB 3085476 A GB3085476 A GB 3085476A GB 1534601 A GB1534601 A GB 1534601A
Authority
GB
United Kingdom
Prior art keywords
hydrazine
july
jet
electrothermal gas
gas thrusters
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.)
Expired
Application number
GB3085476A
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.)
Secretary of State for Defence Canada
UK Secretary of State for Defence
Original Assignee
Secretary of State for Defence Canada
UK Secretary of State for Defence
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 Secretary of State for Defence Canada, UK Secretary of State for Defence filed Critical Secretary of State for Defence Canada
Priority to GB3085476A priority Critical patent/GB1534601A/en
Priority to DE19772733023 priority patent/DE2733023A1/en
Priority to FR7722620A priority patent/FR2359285A1/en
Publication of GB1534601A publication Critical patent/GB1534601A/en
Expired legal-status Critical Current

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
    • F02K9/60—Constructional parts; Details not otherwise provided for
    • F02K9/68—Decomposition chambers

Abstract

1534601 Jet propulsion engines DEFENCE SECRETARY OF STATE FOR 22 July 1977 [23 July 1976] 30854/76 Heading F1J A jet thruster unit, e.g. for controlling space vehicles, comprises a tube 2 electrically heated by coils 3 and containing an injector 8 which directs hydrazine through the central passage 9 of a platinum gauge heat exchanger 7 to impinge against a plate 6, the partially decomposed hydrazine then passing through passages 10 and further gauges 4 to propulsion nozzle 1.
GB3085476A 1976-07-23 1976-07-23 Electrothermal gas thrusters Expired GB1534601A (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
GB3085476A GB1534601A (en) 1976-07-23 1976-07-23 Electrothermal gas thrusters
DE19772733023 DE2733023A1 (en) 1976-07-23 1977-07-21 ELECTROTHERMAL GAS GENERATOR
FR7722620A FR2359285A1 (en) 1976-07-23 1977-07-22 ELECTROTHERMAL ROCKET MOTOR

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3085476A GB1534601A (en) 1976-07-23 1976-07-23 Electrothermal gas thrusters

Publications (1)

Publication Number Publication Date
GB1534601A true GB1534601A (en) 1978-12-06

Family

ID=10314178

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3085476A Expired GB1534601A (en) 1976-07-23 1976-07-23 Electrothermal gas thrusters

Country Status (3)

Country Link
DE (1) DE2733023A1 (en)
FR (1) FR2359285A1 (en)
GB (1) GB1534601A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2007139452A1 (en) * 2006-05-29 2007-12-06 Volvo Aero Corporation Method for fastening of a heater
CN107284638A (en) * 2017-07-17 2017-10-24 海南海大信息产业园有限公司 A kind of annular electromagnetic induction steam jet propeller peculiar to vessel
RU2706101C1 (en) * 2019-01-18 2019-11-13 Федеральное государственное унитарное предприятие "Опытное конструкторское бюро "Факел" ФГУП "ОКБ "Факел" Low-thrust single-component liquid-propellant rocket engine (versions)
RU2717729C2 (en) * 2019-05-24 2020-03-25 Александр Юрьевич Песков Multi-fuel liquid propulsion system operating on single-component propellants
RU2721397C1 (en) * 2019-05-06 2020-05-19 Федеральное государственное унитарное предприятие "Опытное конструкторское бюро "Факел" ФГУП "ОКБ "Факел" Low-thrust single-component liquid-propellant rocket engine

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4461144A (en) * 1981-03-19 1984-07-24 The Secretary Of State For Defence In Her Britannic Majesty's Government Of The United Kingdom Of Great Britain And Northern Ireland Electrothermal gas thrust units
DE3824160A1 (en) * 1988-07-16 1990-01-18 Erno Raumfahrttechnik Gmbh HIGH PERFORMANCE ENGINE
DE19521543C2 (en) * 1995-06-13 1998-02-05 Daimler Benz Aerospace Ag Engine
DE19813330C2 (en) * 1998-03-26 2000-04-13 Daimler Chrysler Ag Process for generating a transverse thrust

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3447316A (en) * 1965-06-07 1969-06-03 Us Navy Radial outflow decomposition chamber
US3377140A (en) * 1965-10-15 1968-04-09 Specialties Dev Corp Apparatus for catalytically decomposing hydrazine
US3772885A (en) * 1968-09-23 1973-11-20 Bolkow Gmbh Method for separation of a fluid monergol for running a rocket motor
US3807657A (en) * 1972-01-31 1974-04-30 Rca Corp Dual thrust level monopropellant spacecraft propulsion system
US3893294A (en) * 1973-09-10 1975-07-08 United Aircraft Corp Catalytic monopropellant reactor with thermal feedback
US3899815A (en) * 1973-09-28 1975-08-19 Rockwell International Corp Thermal bed screen pack
US3956885A (en) * 1974-09-03 1976-05-18 Avco Corporation Electrothermal reactor
GB1473749A (en) * 1975-01-22 1977-05-18 Trw Inc Monopropellant thruster with superheater

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2007139452A1 (en) * 2006-05-29 2007-12-06 Volvo Aero Corporation Method for fastening of a heater
CN107284638A (en) * 2017-07-17 2017-10-24 海南海大信息产业园有限公司 A kind of annular electromagnetic induction steam jet propeller peculiar to vessel
RU2706101C1 (en) * 2019-01-18 2019-11-13 Федеральное государственное унитарное предприятие "Опытное конструкторское бюро "Факел" ФГУП "ОКБ "Факел" Low-thrust single-component liquid-propellant rocket engine (versions)
RU2706101C9 (en) * 2019-01-18 2019-12-23 Федеральное государственное унитарное предприятие "Опытное конструкторское бюро "Факел" ФГУП "ОКБ "Факел" Low-thrust single-component liquid-propellant rocket engine (versions)
RU2721397C1 (en) * 2019-05-06 2020-05-19 Федеральное государственное унитарное предприятие "Опытное конструкторское бюро "Факел" ФГУП "ОКБ "Факел" Low-thrust single-component liquid-propellant rocket engine
RU2717729C2 (en) * 2019-05-24 2020-03-25 Александр Юрьевич Песков Multi-fuel liquid propulsion system operating on single-component propellants

Also Published As

Publication number Publication date
FR2359285B1 (en) 1984-05-11
FR2359285A1 (en) 1978-02-17
DE2733023A1 (en) 1978-02-02

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Legal Events

Date Code Title Description
PS Patent sealed
PCNP Patent ceased through non-payment of renewal fee

Effective date: 19940722