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  • The article deals with the thermal load of the solid propellant booster combustion chamber. In contribution the case of thermal stress of the cylindrical wall is analysed when the solid propellant booster has the short time of action. Thermal stress is a consequence of the solid propellant booster charge burning. For this analyzes the thermal load is estimated from an experiment. The stresses are assessed in the meridional and hoop directions. Cylindrical part of the combustion chamber is closed on one end by the rigid plate and is considered as a shell construction. The pressure and thermal load are axisymmetrical. The new in this paper is evaluation of the thermo camera usage for the temperature fields estimation on the combustion chamber construction during experiments.
  • The article deals with the thermal load of the solid propellant booster combustion chamber. In contribution the case of thermal stress of the cylindrical wall is analysed when the solid propellant booster has the short time of action. Thermal stress is a consequence of the solid propellant booster charge burning. For this analyzes the thermal load is estimated from an experiment. The stresses are assessed in the meridional and hoop directions. Cylindrical part of the combustion chamber is closed on one end by the rigid plate and is considered as a shell construction. The pressure and thermal load are axisymmetrical. The new in this paper is evaluation of the thermo camera usage for the temperature fields estimation on the combustion chamber construction during experiments. (en)
  • Příspěk pojednává o vzniku teplotního zatížení spalovací komory raketového motoru. Je zde analyzován případ vzniku teplotního napětí ve válcové stěně raketového motoru. Teplotní napětí je důsledek hoření náplně raketového motoru na tuhou pohonnou hmotu . Pro analýzu je teplotní pole odhadováno z experimentu. Teplotní pole bylo vyhodnoceno ze snímků termokamery Flir 40. (cs)
Title
  • Contribution to the Solution of thermal Stress in Cylindrical Wall of the Solid Propellant Booster.
  • Contribution to the Solution of thermal Stress in Cylindrical Wall of the Solid Propellant Booster. (en)
  • Příspěvek k řešení teplotního napětí ve válcové stěně pomockého raketového motoru (cs)
skos:prefLabel
  • Contribution to the Solution of thermal Stress in Cylindrical Wall of the Solid Propellant Booster.
  • Contribution to the Solution of thermal Stress in Cylindrical Wall of the Solid Propellant Booster. (en)
  • Příspěvek k řešení teplotního napětí ve válcové stěně pomockého raketového motoru (cs)
skos:notation
  • RIV/60162694:G43__/08:#0001831!RIV09-MO0-G43_____
http://linked.open...avai/riv/aktivita
http://linked.open...avai/riv/aktivity
  • Z(MO0FVT0000404)
http://linked.open...vai/riv/dodaniDat
http://linked.open...aciTvurceVysledku
http://linked.open.../riv/druhVysledku
http://linked.open...iv/duvernostUdaju
http://linked.open...titaPredkladatele
http://linked.open...dnocenehoVysledku
  • 361223
http://linked.open...ai/riv/idVysledku
  • RIV/60162694:G43__/08:#0001831
http://linked.open...riv/jazykVysledku
http://linked.open.../riv/klicovaSlova
  • Solid Propellant Rocket Motor; Combustion Chamber; Thermal Stress (en)
http://linked.open.../riv/klicoveSlovo
http://linked.open...ontrolniKodProRIV
  • [8FD9CF31936C]
http://linked.open...v/mistoKonaniAkce
  • Liptovský Mikuláš
http://linked.open...i/riv/mistoVydani
  • Liptovský Mikuláš (Slovensko)
http://linked.open...i/riv/nazevZdroje
  • Armament and Technics of Land Forces
http://linked.open...in/vavai/riv/obor
http://linked.open...ichTvurcuVysledku
http://linked.open...cetTvurcuVysledku
http://linked.open...UplatneniVysledku
http://linked.open...iv/tvurceVysledku
  • Machala, Milan
http://linked.open...vavai/riv/typAkce
http://linked.open.../riv/zahajeniAkce
http://linked.open...n/vavai/riv/zamer
number of pages
http://purl.org/ne...btex#hasPublisher
  • Akadémia ozbrojených síl geneála M.R. Štefánika
https://schema.org/isbn
  • 978-80-8040-356-0
http://localhost/t...ganizacniJednotka
  • G43
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