Open AccessHow Can Ablative Cooling in A Solid Propellant Rocket Engine Be Accurately Modelled in Order to Optimise Performance?
Author(s) -
Sassan Bhanji
Publication year - 2022
Publication title -
international journal for research in applied science and engineering technology
Language(s) - English
Resource type - Journals
ISSN - 2321-9653
DOI - 10.22214/ijraset.2022.46180
Subject(s) - propellant , aerospace engineering , specific impulse , rocket engine , rocket engine nozzle , thrust , rocket (weapon) , solid fuel rocket , liquid propellant rocket , nozzle , propulsion , mechanical engineering , booster (rocketry) , mechanics , engineering , physics