Atlas is truly a State of the Art development. It represents a leap forward in the realm of personal avionics. Its free form structure and low drag volume allows for optimum flow below wings across the body. It is equipped with a classical airfoil and circular support structures as well as a practice fuselage system. Its greatest strength lies in the optimization of airflow between central body pins and vertical wing interface.

The Modular nature of Atlases components allow for ease of assembly and lean development. In the case of hazard or broken components acquisition and replacement can occur at minimal cost. Flight Data can be found below, along with wind tunnel video.

Titan comes equipped with three main features, wing loft angle optimization, lower body torsion diffusion, and rear support actualization. The wing loft angle is optimized to 2.5 degrees from the horizontal based upon airflow simulation data to generate the most lift. Based on the ultra-light design the lower body torsion minimizes crash error and reconstruction necessities. Finally, the rear support actualization allows for smooth control while airborne and rear flow determination from ground.

There is a number of clear differences between Atlas and Titan. Titan leaves behind the use of low viscosity nano wrap. This is an experimental procedure to explore the airflow and manufacturability of a full filament design. Based upon the data collected from Titan, Mark 3 will be constructed with similar aspect rations and chord lengths but with a more bold deterministic design.