The invention discloses a
propellant charge ignition comprehensive
simultaneity evaluation method. According to the
propellant charge ignition comprehensive
simultaneity evaluation method, sensor supports of fixed sensors are prepared based on the shape of a
propellant chamber and charged propellant structures, the sensors are fixedly arranged on the sensor supports; one terminal of each sensor isarranged on a corresponding sensor support via
welding, is introduced into the propellant chamber, is firmly contacted with the propellant chamber, and is taken as one
signal line terminal, the otherlead of the sensor is fixedly connected with an insulation sealed
electrode on an end cap of the propellant chamber so as to form another
signal line terminal; the propellant is introduced into the propellant chamber; a
pressure release fragment is selected and installed based on
projectile pulling in pressure and propellant charge comprehensive ignition theoretical pressure; igniting and testingare carried out, analysis on test signals is carried out so as to realize evaluation of the ignition comprehensive
simultaneity of propellant charge. The propellant charge ignition comprehensive simultaneity evaluation method is capable of solving test problems in propellant charge ignition effects (simultaneous and comprehensive effect), solving a key technical problem that no scientific
effective method used for evaluation of propellant charge ignition is available, and providing feasible testing and evaluating means for propellant charge design.