The present invention relates to A reduced bleed vapor compression cycle environmental control system for an aircraft. The keys are disposed on an outer surface of the display device, and the microprocessor is disposed inside the display device. One or more of the layers of fibers are penetrated with the prongs, either before or after the fibers have been impregnated with the thermosetting matrix. Operation of the bleed valve enables venting of the coolant from the coolant channels, and through a shut down conduit. A threshold may be determined for each data transmission hypothesized to have been received. A plurality of the compressed data rows are restored in sequence at a high speed so as to reduce the time required for the restoration.