Combined flight control/utility system

Abstract

THE S‐3A VEHICLE is equipped with 2 completely independent hydraulic systems which have been designated as the combined flight control/utility system. These systems are both structurally and hydraulically isolated from each other and are designed and installed in accordance with spec. MIL‐H‐5440 type II (−65° to 275°F temperature range) class 3000 (cutout pressure at pump is 3,100psi).

Citation

(1974), "Combined flight control/utility system", Aircraft Engineering and Aerospace Technology, Vol. 46 No. 3, pp. 12-17. https://doi.org/10.1108/eb035139