RESULTS OF HEAT TRANSFER TESTS OF AN 0.0175-SCALE SPACE SHUTTLE VEHICLE MODEL 22 OTS IN THE NASA-AMES 3.5-FOOT HYPERSONIC WIND TUNNEL (IH3) VOLUME Ⅱ

摘要

Heat-transfer data for the 0.0175-scale Space Shuttle Vehicle 3 are presented in this data report. Interference heating effects were invest igated by a model build-up technique of Orbiter alone, tank alone, second, and first stage configurations.nThe test program was conducted in the NASA-Ames 3.5-Foot Hypertonic Wind Tunnel at Mach 5.3 for nominal free-stream Reynolds number per foot values of 1.5 x 106 and 5.0 x 106.