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GB793689A - Rocket motors - Google Patents

Rocket motors

Info

Publication number
GB793689A
GB793689AGB1711653AGB1711653AGB793689AGB 793689 AGB793689 AGB 793689AGB 1711653 AGB1711653 AGB 1711653AGB 1711653 AGB1711653 AGB 1711653AGB 793689 AGB793689 AGB 793689A
Authority
GB
United Kingdom
Prior art keywords
hydrogen peroxide
fuel
drawn
tank
oxidant
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
GB1711653A
Inventor
Frank Bernard Halford
Arthur Valentine Cleaver
Wilfrid Norwood Neat
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.)
Bristol Siddeley Engines Ltd
Original Assignee
De Havilland Engine Co Ltd
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 DENDAT1070882DpriorityCriticalpatent/DE1070882B/en
Application filed by De Havilland Engine Co LtdfiledCriticalDe Havilland Engine Co Ltd
Priority to GB1711653Aprioritypatent/GB793689A/en
Priority to FR1204592Dprioritypatent/FR1204592A/en
Publication of GB793689ApublicationCriticalpatent/GB793689A/en
Expiredlegal-statusCriticalCurrent

Links

Classifications

Landscapes

Abstract

793,689. Generating combustion products under pressure. DE HAVILLAND ENGINE CO., Ltd. May 25, 1954 [June 19, 1953], No. 17116 /53. Class 51 (1). [Also in Group XXVI] In a rocket motor employing hydrogen peroxide as an oxidant and a liquid fuel, such as kerosine or ammonia, the hydrogen peroxide circulates round the combustion chamber as a coolant and part is subsequently decomposed and supplied to a turbine driving the auxiliary devices. As shown, hydrogen peroxide is drawn from tank 11 by the low-pressure pump 15 and circulated through the cooling spaces 25, 26 of the nozzle 24 and combustion chamber 10 to the high-pressure pump 16 which introduces the oxidant simultaneously to the chamber 10 through the catalyst elements 40 and to the turbine 22 through the catalyst 23. Fuel is drawn from tank 12 by the pump 19 and passes to 10 through the valve 51 which controls the delivery of fuel to injectors 36, 37, 38. Specifications 743,357, [Group XXIX], 792,650, [Group XXVI], and 792,909 are referred to.
GB1711653A1953-06-191953-06-19Rocket motorsExpiredGB793689A (en)

Priority Applications (3)

Application NumberPriority DateFiling DateTitle
DENDAT1070882DDE1070882B (en)1953-06-19 Rocket propulsion
GB1711653AGB793689A (en)1953-06-191953-06-19Rocket motors
FR1204592DFR1204592A (en)1953-06-191958-04-22 Rocket engine

Applications Claiming Priority (1)

Application NumberPriority DateFiling DateTitle
GB1711653AGB793689A (en)1953-06-191953-06-19Rocket motors

Publications (1)

Publication NumberPublication Date
GB793689Atrue GB793689A (en)1958-04-23

Family

ID=10089540

Family Applications (1)

Application NumberTitlePriority DateFiling Date
GB1711653AExpiredGB793689A (en)1953-06-191953-06-19Rocket motors

Country Status (3)

CountryLink
DE (1)DE1070882B (en)
FR (1)FR1204592A (en)
GB (1)GB793689A (en)

Cited By (14)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
DE1095593B (en)*1958-08-191960-12-22Napier & Son Ltd Rocket engine
DE1097764B (en)*1956-07-051961-01-19Bristol Siddeley Engines Ltd Rocket propulsion
DE1138283B (en)*1960-04-121962-10-18United Aircraft Corp Liquid fuel rocket
US3062004A (en)*1959-05-181962-11-06United Aircraft CorpRocket motor starter
DE1164753B (en)*1959-12-121964-03-05Boelkow Entwicklungen Kg Rocket engine for liquid fuels
DE1199542B (en)*1959-06-241965-08-26United Aircraft Corp Device for fuel supply for liquid rockets
US3515040A (en)*1967-06-141970-06-02Bolkow GmbhLiquid fuel rocket engine
US3514953A (en)*1968-10-211970-06-02Us Air ForceTrimode rocket engine
US5697212A (en)*1994-12-271997-12-16Societe Europeenne De PropulsionRocket propellant tank self-pressurization
EP1533511A1 (en)*2003-11-182005-05-25Nederlandse Organisatie Voor Toegepast-Natuurwetenschappelijk Onderzoek TnoProcess for igniting a rocket engine and rocket engine
EP3726011A1 (en)*2019-04-142020-10-21Hamilton Sundstrand CorporationPower module with blow down fuel and propellant delivery system
CN112855381A (en)*2020-12-102021-05-28西安航天动力研究所Space hybrid propulsion system based on photolysis water hydrogen production technology
CN114810428A (en)*2022-03-302022-07-29北京航天动力研究所Precooling device and method for engine hydrogen system under simulation verification flight state
EP4343138A1 (en)*2022-09-262024-03-27ArianeGroup GmbHRocket propulsion, method and spacecraft

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
DE1159695B (en)*1960-12-021963-12-19United Aircraft Corp Propellant control system for a liquid rocket
DE1272636B (en)*1966-08-051968-07-11Boelkow Gmbh Main flow rocket engine
DE1278182B (en)*1966-11-111968-09-19Boelkow Gmbh Formation and mounting of the heat shield in liquid rocket engines in the main flow design
US3722217A (en)*1971-03-031973-03-27Sundstrand CorpAuxiliary hydraulic power supply

Cited By (16)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
DE1097764B (en)*1956-07-051961-01-19Bristol Siddeley Engines Ltd Rocket propulsion
DE1095593B (en)*1958-08-191960-12-22Napier & Son Ltd Rocket engine
US3062004A (en)*1959-05-181962-11-06United Aircraft CorpRocket motor starter
DE1199542B (en)*1959-06-241965-08-26United Aircraft Corp Device for fuel supply for liquid rockets
DE1164753B (en)*1959-12-121964-03-05Boelkow Entwicklungen Kg Rocket engine for liquid fuels
DE1138283B (en)*1960-04-121962-10-18United Aircraft Corp Liquid fuel rocket
US3515040A (en)*1967-06-141970-06-02Bolkow GmbhLiquid fuel rocket engine
US3514953A (en)*1968-10-211970-06-02Us Air ForceTrimode rocket engine
US5697212A (en)*1994-12-271997-12-16Societe Europeenne De PropulsionRocket propellant tank self-pressurization
EP1533511A1 (en)*2003-11-182005-05-25Nederlandse Organisatie Voor Toegepast-Natuurwetenschappelijk Onderzoek TnoProcess for igniting a rocket engine and rocket engine
EP3726011A1 (en)*2019-04-142020-10-21Hamilton Sundstrand CorporationPower module with blow down fuel and propellant delivery system
CN112855381A (en)*2020-12-102021-05-28西安航天动力研究所Space hybrid propulsion system based on photolysis water hydrogen production technology
CN114810428A (en)*2022-03-302022-07-29北京航天动力研究所Precooling device and method for engine hydrogen system under simulation verification flight state
CN114810428B (en)*2022-03-302024-05-31北京航天动力研究所Precooling device and method for simulating and verifying engine hydrogen system under flight state
EP4343138A1 (en)*2022-09-262024-03-27ArianeGroup GmbHRocket propulsion, method and spacecraft
WO2024068395A1 (en)*2022-09-262024-04-04Arianegroup GmbhRocket engine, method and spacecraft

Also Published As

Publication numberPublication date
DE1070882B (en)1959-12-10
FR1204592A (en)1960-01-27

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