UAI–UGATU scientific school of module and vector thrust SRM control
Keywords:
Solid rocket engine fuel; control system; a combustion chamber; nozzle; steering boosterAbstract
The main directions of scientific researches "UGATU" in the field of solid propellant engines founded by professors Z. G. Shaikhutdinov and A.M. Rusak are considered. The results of modern researches of the gas generator characteristics with a pressure control system through the control area of the nozzle throat are discussed. The results of experiments on the combined SRM control method to change the surface area of the combustion space and the nozzle throat are observed.Downloads
Published
2017-20-06
Issue
Section
AIRCRAFT AND ROCKET AND SPACE TECHNOLOGY