NASA NTRS · 19780044557
Approach and landing test supplemental report
Abstract
Tail-cone-off tests of the Shuttle Orbiter during the approach and landing phase are described with attention to attack angle during descent. Angles of from 2.5 to 16.5 deg were attempted with varying speed brake configurations in order to analyze stability and control for runway landings.
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Engle, J. H., Truly, R. H.. 1977-01-01. Approach and landing test supplemental report. https://ntrs.nasa.gov/citations/19780044557
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