Test launch control equipment for small solid rockets or target projectiles

The utility model provides test launch control equipment for a small solid rocket or a target projectile, belongs to the technical field of test launch control, and solves the problems of complex structure, larger size, higher cost and poorer universality of the existing equipment. The device comprises a test launch control shell, and a main control computer, a keyboard-mouse-display all-in-one machine, a distribution box and a photoelectric converter which are integrated in the shell. Test launch control software is configured on the main control computer, a data input end of the test launch control software is connected with a data sensor carried on the rocket or the target missile to be tested, a data output end of the test launch control software is connected with the keyboard-mouse-display all-in-one machine and is accessed to a local area network through a photoelectric converter, and a control signal output end of the test launch control software is connected with electrical equipment on the rocket or