Methodology for full-body TPS sizing of access-to-space vehicles

34th Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1996, Pages

  Milos, F S ^a   Chen, Y K ^a   Henline, W D ^a  

^a NASA AMES RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE VEHICLES; DATABASE SYSTEMS; GRAPHICAL USER INTERFACES; HEAT CONDUCTION; HEAT FLUX; HEAT SHIELDING; HYPERSONIC FLOW; HYPERSONIC VEHICLES; NASA; NAVIER STOKES EQUATIONS; ROCKETS; TEMPERATURE; THERMAL INSULATING MATERIALS;

ACCESS TO SPACE VEHICLES; AERODYNAMIC SIMULATIONS; GENERAL BOUNDARY CONDITIONS; NAVIER-STOKES COMPUTATIONS; SINGLE STAGE TO ORBITS; TEMPERATURE AND PRESSURES; THERMAL PROTECTION SYSTEM; TRANSIENT HEAT CONDUCTION;

AUTOMOBILE BODIES;

EID: 85088199184     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1996-614     Document Type: Conference Paper

References (18)

1. Chen, Y.-K., Henline, W.D., "Analysis of Hypersonic Arcjet Flow Fields and Surface Heating of Blunt Bodies," AIAA Paper 93-0272, Jan. 1993.
2. Chen, Y.-K., Henline, W.D., Stewart, D.A., and Candler, G. V., "Navier- Stokes Solutions with Surface Catalysis for Martian Atmospheric Entry," Journal of Spacecraft and Rockets, Vol. 30, No. 1, 1993, pp. 32-42.
3. Chen, Y.-K., Henline, W.D., "Hypersonic Nonequilibrium Navier-Stokes Solutions Over an Ablating Graphite Nosetip," Journal of Spacecraft and Rockets, Vol. 31, No. 5, 1994, pp. 728-734.
4. Milos, F.S., and Rasky, D.J., "Review of Numerical Procedures for Computational Surface Thermochemistry," Journal of Thermophysics and Heat Transfer, Vol. 8, No. 1, 1994, pp. 24-34.
5. Chen, Y.-K., Henline, W.D., and Tauber, M.E., "MARS Pathfinder Trajectory Based Heating And Ablation Calculations," Journal of Spacecraft and Rockets, Vol. 32, No. 2, 1995, pp. 225-230.
6. Henline, W.D., Palmer, G.E., Chen, Y.-K., Milos, F.S., and Olynick, D.R., "Aerothermodynamic Heating Analysis and Heatshield Design of an SSTO Rocket Vehicle for Access-to-Space," AIAA Paper 95-2079, June 1995.
7. Molvik, G., Milos, F.S., Chen, Y.-K., and Squire, T.H., "Computation of High Speed Flow Fields with Multidimensional Solid Heat Conduction," AIAA Paper 95-2116, June 1995.
8. Chen, Y.-K., and Milos, F.S., "Solution Strategy for Thermal Response of Nonablating Thermal Protection Systems at Hypersonic Speeds," AIAA Paper 96-0615, Jan. 1996.
9. Anon., Access to Space Advanced Technology Team, Final Report, Vol. 1: Executive Summary, NASA, July 1993.
10. Squire, T.H.,TPSX for Windows, Version 1, Thermosciences Institute Report, Sept. 1994.
11. McGrory, D.M., Slack, D.C., Applebaum, M.P., and Walters, R.W., GASP Version 2.2 User's Manual, Aerosoft, 1993.
12. Stewart, D.A., Pallix, J., and Esfahani, L., "Surface Catalytic Efficiency of Candidate Ceramic Thermal Protection Materials, " NASA CDTM-20007, March 1995.
13. Chen, Y.-K., Henline, W.D., Olynick, D.R., and Palmer, G.E., "ThreeDimensional Hypersonic Flowfields and Heating Analysis Over DC-3 Vehicle," AIAA Paper 95-2081, June 1995.
14. Bartlett, E.P., Kendal, R.M., and Rindal, R.A., "An Analysis of the Coupled Chemically Reacting Boundary Layer and Charring Ablator: Part IV - A Unified Approximation for Mixture Transport Properties for Multicomponent Boundary-Layer Application," NASA CR-1063, June 1968.
15. Gupta, R.N., Yos, J.M., Thompson, R.A., and Lee, K., "A Review of Reaction Rates and Thermodynamic and Transport Properties for an 11- Species Air Model for Chemical and Thermal Nonequilibrium Calculations to 30,000 K," NASA Reference Publication 1232, Aug. 1990.
16. Chen, Y.-K., personal communication.
17. Squire, T.H., Tran, H.K., Tran, D., and Kourtides, D.A., "NASP GWP 95: TPS Insulation System Development, Final Report," NASP TM 1204 April 1995.
18. Palmer, G.E., Henline, W.D., Olynick, D.R., and Milos, F.S., "A Heating Analysis and Thermal Protection System Sizing of a Lifting Body Single-Stage-to-Orbit Vehicle," AIAA Paper 95-2080, June 1995.