GB2577133B - Increased scalability expander cycle rocket engine - Google Patents

Increased scalability expander cycle rocket engine Download PDF

Info

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

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

Similar Documents

Publication Publication Date Title
SG11202108231PA (en) Rocket engines
GB201717834D0 (en) Search engine
GB2560949B (en) Split cycle internal combustion engine
GB2558330B (en) Split cycle engine
PL3267024T3 (en) Rocket engine
ZAA201801061S (en) Engines
IL281246A (en) Engine for producing thrust
GB201809661D0 (en) Split cycle engine
GB2581960B (en) Split cycle engine
GB201820918D0 (en) Turbine engine
GB201809068D0 (en) Double acting piston engines
GB201712120D0 (en) Split cycle engine
GB201712111D0 (en) Enhanced combustion engine
GB2577133B (en) Increased scalability expander cycle rocket engine
GB201814887D0 (en) Increased scalability expander cycle rocket engine
GB201814834D0 (en) Increased scalability expander cycle rocket engine
GB2567659B (en) Turbofan engine
GB201806426D0 (en) Turbofan engine
GB2574615B (en) Combustion engine
GB201809659D0 (en) Split cycle engine
EP3622167C0 (en) Hot gas engine having a step piston
GB201805146D0 (en) Turbine engine
GB201708771D0 (en) Improved search engine
GB201809644D0 (en) Thermodynamic engine
ZA201905653B (en) Thermodynamic engine

Legal Events

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

Effective date: 20210505