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Model 47-OTS - Protuberance Balances in their 69Ĭarrying Case with Metric Protuberances Attached Model 47-OTS - Probe Traversing Mechanism 68 Model 47-OTS - Forward Attach Structure Detail 67 Model 47-OTS - Forward Attach Structure 66 Model 47-OTS - Rear Attach Structure Details 65 Model 47-OTS - Closeup of Rear Attach Structure 64 Model 47-OTS - Closeup of probe carrier 63į. Model 47-OTS detail showing traversing probe 62Ĭarrier details and pressure instrumentedĮ. Model 47-OTS in the NASA/ ARC 11x11 foot tunnel 61ĭ. Model 47-OTS in the NASA/ ARC 11x11 foot tunnel 60Ĭ. Model 47-OTS in the NASA/ ARC 11x11 foot tunnel 59ī. Probe Calibration Installation in MSFC 14 M TWT 57Ī.

Metric Protuberance Attachment Details 52.

ET Angular Definitions and Balance Locations 49 Modal Axis Systems and Sign ConventionsĠ. II DATA SET/RUN NUMBER COLLATION SUMMARY 30ġ. Surface centerline to obtain flow field data betweenĭ) Schlieren photographs and ultraviolet flow photographsĭata from each of the four test phases are presented. Mounted on a traversing mechanism on the tank upper Rotated to two positions to yield 128 pressureĬ) Three Chrysler miniature flow direction probes were Line was instrumented with 64 pressure taps and was Pressure taps and was rotated to four positions to The L0 2 feedline was instrumented with 96 To fulfill these objectives the following steps were taken:Ī) Eight 3 -component balances were used to measure forcesī) 315 pressure orifices were distributed over all 9 above

Objective was to obtain structural loads on the following Identified as IA190A/B and was conducted from 7 Feb. Launch vehicle in the NASA/Ames Research Center llxll-foot andĩx7-foot Unitary Plan Wind Tunnels. NATIONAL AERONAUTICS AND SPACE ADMINISTRATIONĭata were obtained on a 3 -percent model of the Space Shuttle NAVIGATION, CONTROL & AERONAUTICS DIVISION

Prepared under NASA Contract Number NAS9-17840 SPACE SHUTTLE LAUNCH CONFIGURATION (MODEL 47-OTS) IN RESULTS OF EXPERIMENTAL INVESTIGATIONS TO DETERMINE

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Full text of " 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, volume 1"