Results of experimental investigations to determine external tank protuberance loads using a 0.03-scale model of the space shuttle launch configuration (model 47-OTS) in the NASA/ARC unitary plan wind tunnel (IA190A/B)
By: by S.R. Houlihan ; prepared under NASA contract number NAS9-17840 by Data Management Services, Chrysler Technologies Airborne Systems, Michoud Engineering Office.
Contributors: Lyndon B. Johnson Space Center. Navigation, Control, & Aeronautics Division.
Series: [NASA contractor report] -- NASA CR-167690, 167691.
Publisher: Navigation, Control, & Aeronautics Division, Johnson Space Center, National Aeronautics and Space Administration
Published: 1992
Place of publication: Houston, Tex
Language: eng
Format: Microform
Subjects: Space shuttles -- Testing.
Other titles: Space shuttle aerothermodynamic data report.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 93-1347-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1993] 7 microfiches.