III.G.13. Compact Kinetic Energy Missile (CKEM) Technology. By FY99, develop and demonstrate technology for an insensitive, lightweight, miniature hypervelocity kinetic energy missile (35-40 kg), which is compatible with the LOSAT target acquisition and tracking system and could be compatible with the fire control system, for close combat and short range air defense missions. Demonstrate the missile KE Penetrator achieving M829A2 equivalent kinetic energy at 175 m and maintaining the energy to beyond 5 km, and achieving greater than 3 times the M829A2 penetrator energy at 450 m and maintaining it to 3.5 km. Demonstrate the missile delivering in excess of 30 MJ to the target at a range of less than 500 meters, as well as a range out to 4 km, and 25 MJ at 5 km. Leverage miniaturized guidance and control actuation technology, high fidelity visual digital simulation, advanced composite motor and structure technology, fire control, insensitivenondetonable propulsion technology, and enhanced lethality characteristics from the LOSAT missile program and the Hypervelocity Missile Guidance STO. Demonstrate increased maneuverability against airborne targets at minimum range with continuous control actuation. Significantly increase missile platform adaptability to include future main battle tanks, helicopters, and multiple lightweight platforms, which are strategically deployable. Demonstrate motor and propulsion concept by FY98, and conduct a flight test in FY98. Demonstration of this miniature hypervelocity missile concept will provide capability for a significant increase in lethality, survivability, and mobility of a dual role close combat and short range air defense hypervelocity guided KE weapon system.
|STO Manager:||TSO:||TRADOC POC:|
|George W. Snyder||Mike Rithmire||COL Arnold J Canada|