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
([NASA contractor report] ; NASA CR-167690, NASA CR-167691)