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Investigation of the Static Longitudinal and Lateral Stability Characteristics of a 0.10-Scale Model of a Three-Stage Configuration of the Scout Research Vehicle at Mach Numbers of 2.29, 2.96, 3.96, and 4.65An investigation w a s made i n the Langley Unitary Plan wind tunnel o determine the effects of fin area and the effects of antennas and w iring tunnels on the static longitudinal and lateral stability of a 0 .10- scale model of a three- stage configuration of the Scout vehicle. The tests were performed at Mach numbers of 2.29, 2.96, 3.96, and 4. 65 6 and at Reynolds numbers of about 3.5 X 10 per foot.
Document ID
20040008066
Acquisition Source
Langley Research Center
Document Type
Other - NASA Technical Note (TN)
Authors
Jernell, Lloyd S. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 21, 2013
Publication Date
March 1, 1961
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
L-1269
NASA-TN-D-711
Report Number: L-1269
Report Number: NASA-TN-D-711
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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