GB2577133B - Increased scalability expander cycle rocket engine - Google Patents

Increased scalability expander cycle rocket engine Download PDF

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Publication number
GB2577133B
GB2577133B GB1815316.3A GB201815316A GB2577133B GB 2577133 B GB2577133 B GB 2577133B GB 201815316 A GB201815316 A GB 201815316A GB 2577133 B GB2577133 B GB 2577133B
Authority
GB
United Kingdom
Prior art keywords
rocket engine
expander cycle
increased scalability
cycle rocket
scalability
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.)
Active
Application number
GB1815316.3A
Other versions
GB201815316D0 (en
GB2577133A (en
Inventor
Desmond Lewis Stephen
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.)
Individual
Original Assignee
Individual
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 claimed from GBGB1814834.6A external-priority patent/GB201814834D0/en
Priority claimed from GBGB1814887.4A external-priority patent/GB201814887D0/en
Application filed by Individual filed Critical Individual
Publication of GB201815316D0 publication Critical patent/GB201815316D0/en
Publication of GB2577133A publication Critical patent/GB2577133A/en
Application granted granted Critical
Publication of GB2577133B publication Critical patent/GB2577133B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • F02K9/44Feeding propellants
    • F02K9/46Feeding propellants using pumps
    • F02K9/48Feeding propellants using pumps driven by a gas turbine fed by propellant combustion gases or fed by vaporized propellants or other gases
    • 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
    • F02K9/08Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/32Constructional parts; Details not otherwise provided for
    • F02K9/40Cooling arrangements
    • 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
    • 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
    • F02K9/46Feeding propellants using pumps
    • 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 not otherwise provided for
    • F02K9/62Combustion or thrust chambers
    • F02K9/64Combustion or thrust chambers having cooling arrangements
    • 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
    • F02K9/97Rocket nozzles
    • F02K9/972Fluid cooling arrangements for nozzles

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
GB1815316.3A 2018-09-12 2018-09-20 Increased scalability expander cycle rocket engine Active GB2577133B (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GBGB1814834.6A GB201814834D0 (en) 2018-09-12 2018-09-12 Increased scalability expander cycle rocket engine
GBGB1814887.4A GB201814887D0 (en) 2018-09-13 2018-09-13 Increased scalability expander cycle rocket engine

Publications (3)

Publication Number Publication Date
GB201815316D0 GB201815316D0 (en) 2018-11-07
GB2577133A GB2577133A (en) 2020-03-18
GB2577133B true GB2577133B (en) 2021-03-24

Family

ID=64024224

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1815316.3A Active GB2577133B (en) 2018-09-12 2018-09-20 Increased scalability expander cycle rocket engine

Country Status (1)

Country Link
GB (1) GB2577133B (en)

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20030136111A1 (en) * 2002-01-22 2003-07-24 Hy Pat Corporation Hybrid rocket motor using a turbopump to pressurize a liquid propellant constituent
US20180038316A1 (en) * 2016-08-02 2018-02-08 Orbital Atk, Inc. Liquid-fueled rocket engine assemblies, and related methods of using liquid-fueled rocket engine assemblies

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20030136111A1 (en) * 2002-01-22 2003-07-24 Hy Pat Corporation Hybrid rocket motor using a turbopump to pressurize a liquid propellant constituent
US20180038316A1 (en) * 2016-08-02 2018-02-08 Orbital Atk, Inc. Liquid-fueled rocket engine assemblies, and related methods of using liquid-fueled rocket engine assemblies

Also Published As

Publication number Publication date
GB201815316D0 (en) 2018-11-07
GB2577133A (en) 2020-03-18

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Legal Events

Date Code Title Description
746 Register noted 'licences of right' (sect. 46/1977)

Effective date: 20210505