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) [microform] / by S.R. Houlihan ; prepared under NASA contract number NAS9-17840 by Data Management Services, Chrysler Technologies Airborne Systems, Michoud Engineering Office

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