0.4 Percent Scale Space Launch System Wind Tunnel Test
0.4 Percent Scale Space Launch System Wind Tunnel Test 0.4 Percent Scale SLS model installed in the NASA Langley Research Center Unitary Plan Wind Tunnel Test Section 1 for aerodynamic force and movement testing.
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Details
NASA ID
LRC-2011-04062
Date Created
November 15, 2011
Center
LRC
Media Type
image
Photographer
George Homich
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