Open AccessEstimation Methods for Turbine Nozzle Throat Area Reduction of A LOx/Kerosene Gas Generator Cycle Liquid Propellant Rocket Engine
Author(s) -
Chang-Ho Nam,
Young Ho Moon,
Soon Young Park,
Jinhan Kim
Publication year - 2019
Publication title -
han'gug cujin gonghag hoeji/han-guk chujin-gong hakoeji
Language(s) - English
Resource type - Journals
eISSN - 2288-4548
pISSN - 1226-6027
DOI - 10.6108/kspe.2019.23.5.101
Subject(s) - propellant , kerosene , nozzle , liquid propellant rocket , gas generator , rocket engine nozzle , rocket (weapon) , gas turbines , aerospace engineering , liquid oxygen , generator (circuit theory) , reduction (mathematics) , turbine , automotive engineering , environmental science , materials science , engineering , mechanical engineering , power (physics) , chemistry , physics , mathematics , thermodynamics , geometry , organic chemistry , oxygen