The total project objective is to develop a projectile that extends its range without a rocket motor via optimal oblique-wing aerodynamic gliding. It should weigh about as much as the Extended Range Guided Munition (ERGM), have the same length, must survive the same g-load (~12,500 g's), and have a warhead volume that is 20% greater than the ERGM.. Its goal is to achieve the threshold range of 63nm, preferably 100nm, within ten minutes. The Phase II deliverable is a paper preliminary/detailed design of a gun-launched Arizona Glider (GLAG or AG). The phase II effort includes: 1) Down-select a well-defined AG configuration; 2) Intensive CFD computation to establish a viable aerodynamic database; 3) Complete preliminary and detailed design phases for the AG in which component designs such as wing attachment/actuation, control surface and smart actuation, and g-hardening must be resolved; 4) Fully develop a 6 DOF simulation program to assess the AG performance. The phase II option will be to set up plans and design AG models for wind tunnel test and drop tests in preparation for phase III. The ZONA team consists of ZONA Technology, CAES, AeroVironment, and OSU, a versatile, well-experienced team that will work closely with NSWC personnel to achieve the challenging goal.