The invention provides an autonomous separation universal controlled 
projectile body for a 40mm 
rocket launcher. A control cabin, an electric steering engine, a guidance guiding or receiving 
assembly,an autonomous separation mechanism and a foldable skirt 
tail mechanism are additionally arranged; the control cabin, the electric steering engine and the autonomous separation mechanism are connectedin sequence and located on a super-
caliber cabin section, and the super-
caliber cabin section is fixedly connected with the 
projectile body located in the 
rocket launcher through the autonomous separation mechanism; the guidance guiding or receiving 
assembly is located in the autonomous separation mechanism, the foldable skirt 
tail mechanism is installed at the front end of the autonomous separation mechanism, and the foldable skirt 
tail mechanism is limited by the autonomous separation mechanism to be in a folded state before the 
projectile body is launched; after the projectile body is launched, the super-
caliber cabin section is separated from the projectile body located in the 
rocket launcher through the autonomous separation mechanism, the guidance guiding or receiving 
assembly is exposed, and the foldable skirt tail mechanism is unfolded; and the control cabin completes calculation and generates a control instruction to drive the electric steering engine so as to control the controlled projectile body to fly. According to the autonomous separation universal controlled projectile body for the 40mm rocket launcher provided by the invention, the shielding influence of a rear-section projectile body structure on a guidance 
signal in the subsequent 
flight process of a guided 
missile can be avoided.