Potentiometer/resistor made by Aerojet General Corp. for use with linear transducer as part of the pneumatic control system of the propellent control valve of the AJ10-137 rocket engine, as used in the Apollo Service Module's service propulsion system. The component measures approximately 3″ x 5″ x 1.75″ and is marked on the side: "Resistor, Variable, Dual, 2000 Ω, 0.5 W, Travel 1.75 Inches." Accompanied by copies of diagrams demonstrating the location of the potentiometer/resistor in the Apollo SPS engine.
We use cookies on this site to improve your experience. By using this site, you accept our use of cookies. To learn more, please see our Privacy Policy.