For passive flow rate control of oxidizer and fuel of a liquid propellant engine a cavitating venturi is designed, produced and tested.
Passive flow rate control of the fuel and the oxidizer in liquid fuelled rocket motors
2005-01-01
536769 byte
Conference paper
Electronic Resource
English
Intelligent control of liquid-fuelled bi-propellant premix rocket motors
British Library Conference Proceedings | 2006
|A numerical investigation of oxidizer mixed hybrid rocket motors
Online Contents | 2015
|A numerical investigation of oxidizer mixed hybrid rocket motors
Elsevier | 2015
|