Open AccessCONTOUR DESIGN FOR SOLID-PROPELLANT ROCKET-ENGINE NOZZLE
Author(s) -
Minh Phú Nguyễn
Publication year - 2020
Publication title -
kỹ thuật quân sự
Language(s) - Uncategorized
Resource type - Journals
ISSN - 1859-0209
DOI - 10.56651/lqdtu.jst.v15.n01.105
Subject(s) - nozzle , propellant , rocket engine nozzle , rocket (weapon) , thrust , rocket engine , aerospace engineering , missile , range (aeronautics) , solid fuel rocket , contour line , propulsion , mechanical engineering , liquid propellant rocket , mechanics , materials science , engineering , physics , meteorology