Control systems are necessary in rocket engines to regulate parameters (such as pressure in the combustion chamber, thrust magnitude and direction, and propellant mixture ratio and consumption) during normal engine operation and also during start-up and shut-down transients. The principal actuators used for control functions (such as valves, regulators, pressure switches, and flow controls) are described here.
Control Systems and Valves
Springer Aerospace Techn.
2020-09-27
116 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
Fuel Level Control Valves/Systems
SAE Technical Papers | 2007
Fuel level control valves/systems
TIBKAT | 1997
Fuel Level Control Valves/Systems
SAE Technical Papers | 1981
FUEL LEVEL CONTROL VALVES/SYSTEMS
SAE Technical Papers | 1987
Fuel Level Control Valves and Systems
SAE Technical Papers | 2021