Skoll Flight 2

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https://hdl.handle.net/11299/172727

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Title

Skoll Flight 2

Authors

Taylor, Brian

Published Date

2015-06-23

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Abstract

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Skoll Flight 2

UMore Test Range

Rigid Body Aerodynamics

Description

The goal for this flight was to obtain rigid body aerodynamic data for Skoll. The second flight failed to launch immediately at 35 knots, upon safeing the launcher the aircraft released. Again the aircraft rolled hard left. The pilot recovered from the ensuing stall and got the aircraft turned for landing crossfield. Final approach was very stable, near the ground the nose pitched up rapidly. The end result was a hard impact on the nose.

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Taylor, Brian. (2015). Skoll Flight 2. Retrieved from the University Digital Conservancy, https://hdl.handle.net/11299/172727.

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