GB2518211B - Rocket motor with combustion chamber having porous membrane - Google Patents

Rocket motor with combustion chamber having porous membrane

Info

Publication number
GB2518211B
GB2518211B GB1316343.1A GB201316343A GB2518211B GB 2518211 B GB2518211 B GB 2518211B GB 201316343 A GB201316343 A GB 201316343A GB 2518211 B GB2518211 B GB 2518211B
Authority
GB
United Kingdom
Prior art keywords
combustion chamber
porous membrane
rocket motor
rocket
motor
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 - Fee Related
Application number
GB1316343.1A
Other versions
GB2518211A (en
GB201316343D0 (en
Inventor
Carolyn Billie Knight
Geoffrey Daly
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
Application filed by Individual filed Critical Individual
Priority to GB1316343.1A priority Critical patent/GB2518211B/en
Publication of GB201316343D0 publication Critical patent/GB201316343D0/en
Publication of GB2518211A publication Critical patent/GB2518211A/en
Application granted granted Critical
Publication of GB2518211B publication Critical patent/GB2518211B/en
Expired - Fee Related 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
    • F02K9/08—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
    • F02K9/34—Casings; Combustion chambers; Liners thereof
    • 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
    • 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
    • F02K9/974—Nozzle- linings; Ablative coatings
    • 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
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/50—Intrinsic material properties or characteristics
    • F05D2300/514—Porosity

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Spray-Type Burners (AREA)
GB1316343.1A 2013-09-13 2013-09-13 Rocket motor with combustion chamber having porous membrane Expired - Fee Related GB2518211B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1316343.1A GB2518211B (en) 2013-09-13 2013-09-13 Rocket motor with combustion chamber having porous membrane

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1316343.1A GB2518211B (en) 2013-09-13 2013-09-13 Rocket motor with combustion chamber having porous membrane

Publications (3)

Publication Number Publication Date
GB201316343D0 GB201316343D0 (en) 2013-10-30
GB2518211A GB2518211A (en) 2015-03-18
GB2518211B true GB2518211B (en) 2015-11-18

Family

ID=49552638

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1316343.1A Expired - Fee Related GB2518211B (en) 2013-09-13 2013-09-13 Rocket motor with combustion chamber having porous membrane

Country Status (1)

Country Link
GB (1) GB2518211B (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2018075105A1 (en) * 2016-07-12 2018-04-26 Additive Rocket Corporation Regenerative hybrid rocket motor

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB780433A (en) * 1954-09-27 1957-07-31 Power Jets Res & Dev Ltd Flame tubes and other ducts made of fluid-permeable metal sheet
US3719046A (en) * 1970-07-02 1973-03-06 Rocket Research Corp Rocket engine cooling system
EP0401107A1 (en) * 1989-05-29 1990-12-05 Societe Europeenne De Propulsion (S.E.P.) S.A. Combustion chamber for ram jet
US20020069636A1 (en) * 1999-03-24 2002-06-13 Knuth William H. Hybrid rocket engine and method of propelling a rocket
US20040128980A1 (en) * 2002-03-04 2004-07-08 Max Calabro Rocket engine

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB780433A (en) * 1954-09-27 1957-07-31 Power Jets Res & Dev Ltd Flame tubes and other ducts made of fluid-permeable metal sheet
US3719046A (en) * 1970-07-02 1973-03-06 Rocket Research Corp Rocket engine cooling system
EP0401107A1 (en) * 1989-05-29 1990-12-05 Societe Europeenne De Propulsion (S.E.P.) S.A. Combustion chamber for ram jet
US20020069636A1 (en) * 1999-03-24 2002-06-13 Knuth William H. Hybrid rocket engine and method of propelling a rocket
US20040128980A1 (en) * 2002-03-04 2004-07-08 Max Calabro Rocket engine

Also Published As

Publication number Publication date
GB2518211A (en) 2015-03-18
GB201316343D0 (en) 2013-10-30

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Legal Events

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

Effective date: 20210913