Evaluation of an electronic scanner of pressure (ESOP) module

An electronic scanner of pressure (ESOP) module, developed by NASA Ames Research Center, was installed in a wind tunnel and evaluated over a 5-month testing period. The solid-state ESOP module has 48 miniature pressure transducers and a heater circuit to maintain a constant module temperature. During the wind tunnel test, the module was subjected to an environmental temperature range from 60 F to 104 F, and to considerable module vibration. Zero drift was within + or - 0.5 percent of full-scale output for 37 of the transducers, and was greater than 5.0 percent for four transducers. Pressure measurements from 12 transducers were compared with Scanivalve modules. The agreement of these measurements was considered to be good.