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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 (IA-310)

Author(s):
Collette, J.G.R. ( Rockwell International Corp. )  
Publication title:
NASA Technical Reports
Pub. Year:
1991
Issue:
NASA-CR-1676697
No.:
G3/16 0062355
Pt.:
NAS 1.26:1676697
Paper no.:
N92-17214
Page(from):
1
Page(to):
685
Pages:
685
Pub. info.:
National Aeronautics and Space Adminstration
Language:
English
Type:
Technical Paper

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