Trident 2E Aircraft Systems: Details of fuel system, electrical power installation, hydraulic system, air conditioning and pressurisation and flying controls

Abstract

AS is to be expected, the various systems on the Trident 2E closely follow those evolved for the Tridents 1 and 1E, except for the changes in the fuel system necessitated by the introduction of the fin fuel tank, and the embodiment of a turbine‐compressor type of cold air unit in the air conditioning system.

Citation

(1969), "Trident 2E Aircraft Systems: Details of fuel system, electrical power installation, hydraulic system, air conditioning and pressurisation and flying controls", Aircraft Engineering and Aerospace Technology, Vol. 41 No. 4, pp. 14-24. https://doi.org/10.1108/eb034492