The invention provides a device for measuring a class of discontinuous parameters of a
solid rocket engine. The device for measuring the class of discontinuous parameters of the
solid rocket engine comprises a case, an input panel with an input interface socket, a power supply switch and state indication, an output panel with an output interface socket, a power supply socket and a power supply diverter switch, a power supply patch core and a circuit board. A current limitation circuit of the circuit board is formed by connecting
n channel measuring circuits in parallel and then connecting the
n channel measuring circuits with a
total current limitation
resistor R0 in series. A power supply indication circuit of the circuit board is formed by connecting an ordinary luminous
diode L and a power supply indication circuit
resistor R1 in series. A single channel measuring circuit is formed by connecting a highlight luminous
diode Li, a single blade switch K and a one-way
shunting resistor R in series. According to the device for measuring the class of discontinuous parameters of the
solid rocket engine, the luminous
diode is used for observing each line of signals,
current limiting measures are adopted to ensure that the current of each line of the signals is in the
milliampere level, a BNC contact is used for unitizing and simplifying the switch over links, two power supply
modes which are a battery mode and a power supply mode are provided, and therefore measurement of the class of discontinuous parameters in a solid
rocket engine test can be achieved.