Aerospace Instrument-Making Annotation << Back Influencing of thermal effects on the pressure transducer for space flight vehicles В.Э. Джашитов, В.М. Панкратов, В.И. Улыбин и др. The liquid and gaseous mediums pressure transducers in space-rocket engineering operating in non-steady, inhomogeneous temperature fields of measured medium and environment are esteemed. The mathematical models of non-steady thermal processes that are flowing past in considered types of sensors and mathematical models of thermo elastic tight-strained state of diaphragms of detectors of sensors are constructed and are studied. The solution of these problems and their implementation in complexes of the programs allow on a design stage to analyze automatically influence of composite thermal effects on pressure transducers and to work out the guidelines on parameters optimization of these devices.