Missile body recovery system after assessment flight test

The invention provides a missile body recovery system after an assessment flight test. The system comprises a recovery control module, an electric control module and a recovery device. The recovery system is characterized in that a missile enters a speed threshold which cannot be self-stabilized and controlled after completing assessment flight, the recovery control module identifies the speed threshold which is triggered by the current missile and cannot be self-stabilized and controlled, transferring to a recovery system working flight control program is performed, a recovery device startinginstruction is sent to the electric control module, then a missile flight state is monitored, whether the current missile flight state is suitable for switching to the main recovery mode is determined, and a switching instruction is sent to the electric control module once the current missile flight state is suitable for switching to the main recovery mode; the electric control module executes corresponding ignition acco