GB1024279A - Thrust chamber - Google Patents

Thrust chamber

Info

Publication number
GB1024279A
GB1024279A GB112363A GB112363A GB1024279A GB 1024279 A GB1024279 A GB 1024279A GB 112363 A GB112363 A GB 112363A GB 112363 A GB112363 A GB 112363A GB 1024279 A GB1024279 A GB 1024279A
Authority
GB
United Kingdom
Prior art keywords
combustion chamber
segments
chamber
combustion
radially outwardly
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
GB112363A
Other languages
English (en)
Inventor
Alois Thomas Sutor
Thomas Edward Cowell
Robert Samuel Kraemer
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.)
North American Aviation Corp
Original Assignee
North American Aviation Corp
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 NL288688D priority Critical patent/NL288688A/xx
Priority to BE627801D priority patent/BE627801A/xx
Application filed by North American Aviation Corp filed Critical North American Aviation Corp
Priority to GB112363A priority patent/GB1024279A/en
Priority to FR923373A priority patent/FR1350964A/fr
Priority to DEN22683A priority patent/DE1219288B/de
Publication of GB1024279A publication Critical patent/GB1024279A/en
Expired legal-status Critical Current

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
    • F02K9/97Rocket nozzles

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Testing Of Engines (AREA)
GB112363A 1963-01-10 1963-01-10 Thrust chamber Expired GB1024279A (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
NL288688D NL288688A (ru) 1963-01-10
BE627801D BE627801A (ru) 1963-01-10
GB112363A GB1024279A (en) 1963-01-10 1963-01-10 Thrust chamber
FR923373A FR1350964A (fr) 1963-01-10 1963-01-31 Chambre de poussée à écoulement horizontal pour moteurs à fusée
DEN22683A DE1219288B (de) 1963-01-10 1963-02-01 Schubkammer fuer Raketentriebwerke

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB112363A GB1024279A (en) 1963-01-10 1963-01-10 Thrust chamber

Publications (1)

Publication Number Publication Date
GB1024279A true GB1024279A (en) 1966-03-30

Family

ID=9716555

Family Applications (1)

Application Number Title Priority Date Filing Date
GB112363A Expired GB1024279A (en) 1963-01-10 1963-01-10 Thrust chamber

Country Status (3)

Country Link
BE (1) BE627801A (ru)
GB (1) GB1024279A (ru)
NL (1) NL288688A (ru)

Also Published As

Publication number Publication date
BE627801A (ru)
NL288688A (ru)

Similar Documents

Publication Publication Date Title
US2943821A (en) Directional control means for a supersonic vehicle
US3041824A (en) Propulsion system
GB1048645A (en) Aerodynamic or hydrodynamic servo-valve, especially for use for the guidance and stabilisation of rockets
GB1421719A (en) Ramjet powered missiles
GB1102625A (en) Stabilisation and guidance device for sounding rockets and rocket-propelled ballistic vehicles
GB982440A (en) Rocket propelled missile
GB1009269A (en) Improvements in or relating to aircraft
GB1179788A (en) Variable Area Exhaust Deflection System for a Gas Turbine Engine
GB1019303A (en) Improvements in nozzle systems of jet propulsion engines
GB1139005A (en) Improvements in or relating to gas turbine by-pass engines
GB1161949A (en) Improvements in Aircraft Gas Generator Exhaust Nozzle Structures
GB1204268A (en) An exhaust arrangement for a jet engine
GB1024279A (en) Thrust chamber
GB1101663A (en) Variable area nozzles for jet propulsion engines
GB1192887A (en) Swivelable Exhaust Deflection apparatus for Afterburning Gas Turbines Engines
GB1073458A (en) Improvements relating to by-pass ducted for gas-turbine aircraft engines
GB1088153A (en) Improvements in thrust deflecting mechanism
GB985229A (en) Rocket
GB1311292A (en) Propulsion nozzles
GB1038485A (en) Jet propulsion power plant
GB1142660A (en) Improvements in combination jet exhaust nozzle and thrust reverser
GB997943A (en) Fluid curtains for protecting or shielding a body
GB961001A (en) Improvements in propulsion units having a plurality of reaction propulsion nozzles
GB1460142A (en) Missile nozzle configuration
GB885489A (en) Improvements in rocket motors