X-33 metallic TPS tests in NASA-LARC high temperature tunnel

37th Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1999, Pages

  Bouslog, Stanley A ^a   Moore, Brad ^a   Lawson, Irwin ^a   Sawyer, James Wayne ^b  

^a BFGoodrich Aerospace   (United States)

^b NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; ATMOSPHERIC TEMPERATURE;

FLIGHT VEHICLES; HIGH TEMPERATURE; OFF DESIGNS; PRESSURE LOAD; SURFACE TEMPERATURES; THERMAL DATA; THERMAL MODEL; THERMAL PROTECTION SYSTEM;

NASA;

EID: 84983123743     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (4)

1. Sawyer, J. W., Hodge, J, and Moore, B., “Aerothermal Test of Metallic TPS for X-33 Reusable Launch Vehicle,” 3rd European Workshop on Thermal Protection Systems, March 25-27, 1998.
2. Moore, B., “Aerothermal Testing of X-33 Windward Thermal Protection System in the NASA LaRC 8 ft. High Temperature Tunnel,” BF Goodrich Aerospace Report No. RHR 98044, Dec. 1998.
3. Deveikis, W. D. and Hunt, L. R., “Loading and Heating of a Large Flat Plate at Mach 7 in the Langley 8-foot High-Temperature Structures Tunnel,” NASA TN D-7275, Sept. 1973.
4. Cullimore, B. A. and Ring, S. G., “SINDA/FLUINT: Systems Improved Numerical Differencing Analyzer and Fluid Integrator, Ver. 2.5,” Cosmic Program # MSC-21528.