Many of the UAV's developed for NASA's Environmental Research Aircraft and Sensor Technology Program are light weight, have long wingspans and low wing loading. As a result, these UAVs are relatively sensitive to ground winds and in-flight turbulence. The Pathfinder-plus and Helios Prototype have increased risk of damage on the ground if surface winds exceed 7 knots. In flight, control of these vehicles is also threatened in the presence of low altitude turbulence caused by wind shear or thermal activity.
This paper describes how data from the SODAR have impacted UAV flight day activities, including how the data are used to advise UAV flight crews and NASA Mission Directors on current and projected conditions. On one mission the flight time of the X-38 was moved up almost two hours due to the detection of high winds (greater than 20 knots) by the SODAR at altitudes at and above 300 feet AGL. The change in time was necessary to give ground personnel time to safely stow the parafoil before the winds increased above guidelines. Aircraft that will be discussed include Pathfinder-plus, Helios Prototype, Darkstar and the X-38 prototype of the International Space Station's "crew recovery vehicle."