3 edition of Results of the Space Shuttle Vehicle Ascent Air Data System probe calibration test using a 0.07-scale external tank forebody model (68T) in the AEDC 16-foot transonic wind tunnel (I.A.-310). found in the catalog.
Results of the Space Shuttle Vehicle Ascent Air Data System probe calibration test using a 0.07-scale external tank forebody model (68T) in the AEDC 16-foot transonic wind tunnel (I.A.-310).
1991 by National Aeronautics and Space Administration, Lyndon B. Johnson Space Center, National Technical Information Service, distributor in Houston, Tex, [Springfield, Va.? .
Written in English
|Statement||by J.G.R. Collette.|
|Series||NASA-CR -- 167,696., NASA contractor report -- NASA CR-167696.|
|Contributions||Lyndon B. Johnson Space Center.|
|The Physical Object|
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