Engineering topics
Publications and source records attributed to Keltz, W. L..
Design of attitude control system for a sounding rocket is established by using a control loop which incorporates a lead network to convert position output into a feedback signal that is approximately proportional to position, plus a constant times rate.
Design, development, fabrication, and acceptance test results for two fluidic proportional thrusters for use in SPARCS 4
High performance reaction pointing control systems for sounding rockets, using proportional control of differential thrust and adaptive control of thrust magnitude
Fluidic roll control for Aerobee rocket vehicle
Fluidic proportional thrust control system with vortex valves