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).
By: by J.G.R. Collette.
Contributors: Lyndon B. Johnson Space Center.
Series: NASA-CR -- 167,696.; NASA contractor report -- NASA CR-167696.
Publisher: National Aeronautics and Space Administration, Lyndon B. Johnson Space Center; National Technical Information Service, distributor
Published: 1991
Place of publication: Houston, Tex; [Springfield, Va.?
Language: eng
Format: Microform
Subjects: Space shuttles.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 92-2659-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration], 1992. 7 microfiches.