02115nam 2200481 450 991070997290332120180824115948.0(CKB)5470000002474535(OCoLC)1049803362(EXLCZ)99547000000247453520180824j198503 ua 0engur|||||||||||txtrdacontentcrdamediacrrdacarrierResults of aeroheating DFI and ET design-data test on a 0.0175-scale model 60-OTS conducted in the Von Karman gas dynamics facility (VKF) 40-inch supersonic and the 50-inch hypersonic wind tunnels A & C (IH-97A/B/C) /J. MarroquinHouston, Texas :Systems Engineering Division, Johnson Space Center, National Aeronautics and Space Administration,March 1985.1 online resource (iv, 164 pages) illustrationsNASA/CR ;167693"March 1985.""DMS-DR-2520."Includes bibliographical references (page 37).Results of aeroheating DFI and ET design-data test on a 0.0175-scale model 60-OTS conducted in the Von Karman gas dynamics facility Wind tunnel testsnasatAerodynamic heatingnasatExternal tanksnasatSpace shuttlesnasatMach numbernasatWind tunnel tests.Aerodynamic heating.External tanks.Space shuttles.Mach number.Marroquin J.1392908Lyndon B. Johnson Space Center.Systems Engineering Division,Chrysler Corporation.Electronics Products Division.Michoud Engineering Office.Data Management Services.GPOGPOBOOK9910709972903321Results of aeroheating DFI and ET design-data test on a 0.0175-scale model 60-OTS conducted in the Von Karman gas dynamics facility (VKF) 40-inch supersonic and the 50-inch hypersonic wind tunnels A & C (IH-97A3448434UNINA