摘要: IN aircraft close-in-combat scenarios, a large off-boresight angle targeting capability, or the ability to engage targets in the rear hemisphere, is a signifi cant advantage. Superagility in missiles refers to this capability. Following a successful missile launch and separation, dynamic pressures are often too low for aerodynamic controls to make a quick turn. When the propulsion system ignites, vectoring the thrust (or using reaction jets) can provide this capability, and as the velocity increases, the aerodynamic surfaces become more effective …