-
1
-
-
0006093456
-
-
NASA TM 110440
-
Tran, H. K., Johnson, C.E., Rasky, D.J., Hui, F.C., Hsu, M.T., Chen, T., Chen, Y.K., Paragas, D., and Kobayashi, L., "Phenolic Impregnated Carbon Ablators (PICA) as Thermal Protection Systems for Discovery Missions," NASA TM 110440, 1997.
-
(1997)
Phenolic Impregnated Carbon Ablators (PICA) as Thermal Protection Systems for Discovery Missions
-
-
Tran, H.K.1
Johnson, C.E.2
Rasky, D.J.3
Hui, F.C.4
Hsu, M.T.5
Chen, T.6
Chen, Y.K.7
Paragas, D.8
Kobayashi, L.9
-
2
-
-
0032652865
-
Analysis of Galileo probe heat shield ablation and temperature data
-
Milos, F., Chen, W.K., Squire, T. and Brewer, R., "Analysis of Galileo Probe Heat Shield Ablation and Temperature Data," Journal of Spacecraft and Rockets, Vol. 36, No. 3, 1999, pp 298-306.
-
(1999)
Journal of Spacecraft and Rockets
, vol.36
, Issue.3
, pp. 298-306
-
-
Milos, F.1
Chen, W.K.2
Squire, T.3
Brewer, R.4
-
3
-
-
77958486935
-
-
AIAA Paper No. 2009-4230, June
-
Driver, D., M., Carballo, E.,J., Beck, R.A.S., Prabhu, D., Santos, J., Cassell, A., Skokova, K., Hwang, H. H., Slimko, E., Willcockson, W., Songer, J., "Arc Jet Testing in Shear Environment for Mars Science Laboratory Thermal Protection System," AIAA Paper No. 2009-4230, June 2009.
-
(2009)
Arc Jet Testing in Shear Environment for Mars Science Laboratory Thermal Protection System
-
-
Driver, D.M.1
Carballo, E.J.2
Beck, R.A.S.3
Prabhu, D.4
Santos, J.5
Cassell, A.6
Skokova, K.7
Hwang, H.H.8
Slimko, E.9
Willcockson, W.10
Songer, J.11
-
4
-
-
77958465114
-
-
AIAA Paper No. 2009-4231, June
-
Wright, M.,J., Beck, R.,A.,S., Edquist, K.T., Driver, D., M., Sepka, S., Slimko, E., Willcockson, W., DeCaro, A., Hwang, H., H., "Sizing and Margins Assessment of the Mars Science Laboratory Aeroshell Thermal Protection System," AIAA Paper No. 2009-4231, June 2009.
-
(2009)
Sizing and Margins Assessment of the Mars Science Laboratory Aeroshell Thermal Protection System
-
-
Wright, M.J.1
Beck, R.A.S.2
Edquist, K.T.3
Driver, D.M.4
Sepka, S.5
Slimko, E.6
Willcockson, W.7
DeCaro, A.8
Hwang, H.H.9
-
5
-
-
0032637766
-
Ablation and thermal response program for spacecraft heatshield analysis
-
Chen, Y.,-K., and Milos, F. S., "Ablation and Thermal Response Program for Spacecraft Heatshield Analysis," Journal of Spacecraft and Rockets, Vol. 36, No. 3, 1999, pp 475-483.
-
(1999)
Journal of Spacecraft and Rockets
, vol.36
, Issue.3
, pp. 475-483
-
-
Chen, Y.-K.1
Milos, F.S.2
-
6
-
-
77958492241
-
-
AIAA paper 2008-1202, Jan.
-
Stackpoole, M., Sepka, S., Cozmuta, I., and Kontinos, D., "Post-Flight Evaluation of Stardust Sample Return Capsule Forebody Heatshield Material," AIAA paper 2008-1202, Jan 2008.
-
(2008)
Post-Flight Evaluation of Stardust Sample Return Capsule Forebody Heatshield Material
-
-
Stackpoole, M.1
Sepka, S.2
Cozmuta, I.3
Kontinos, D.4
-
9
-
-
0000737072
-
Data-parallel line relaxation method of the Navier-Stokes equations
-
Wright, M. J., Candler, G. V., and Bose, D., "Data-Parallel Line Relaxation Method of the Navier-Stokes Equations," AIAA Journal, Vol. 36, No. 9, 1998, pp., 1603-1609.
-
(1998)
AIAA Journal
, vol.36
, Issue.9
, pp. 1603-1609
-
-
Wright, M.J.1
Candler, G.V.2
Bose, D.3
-
10
-
-
78649888647
-
-
NASA CR-54757
-
Rindal, R. A., Flood, D. T., and Kendall, R. M., "Analytic and Experimental Study of Ablation Material for Rocket-Engine Application," NASA CR-54757, 1966.
-
(1966)
Analytic and Experimental Study of Ablation Material for Rocket-Engine Application
-
-
Rindal, R.A.1
Flood, D.T.2
Kendall, R.M.3
-
11
-
-
0042938945
-
-
NASA CR 1060
-
Kendall, R. M., Bartlett, E. P., Rindal, R. A., and Moyer, C.B., ""An Analysis of the Coupled Chemically Reacting Boundary Layer and Charring Ablator: Part I," NASA CR 1060, 1968.
-
(1968)
An Analysis of the Coupled Chemically Reacting Boundary Layer and Charring Ablator: Part I
-
-
Kendall, R.M.1
Bartlett, E.P.2
Rindal, R.A.3
Moyer, C.B.4
-
12
-
-
0037497709
-
-
NASA CR-1063, June
-
Bartlett, E. P., Kendall, R. M., Rindal, R. A., "An Analysis of a Chemically Reacting Boundary Layer and Charring Ablator: Part IV A Unified Approximation for Mixture Transport Properties for Multi-Component Boundary Layer Calculations," NASA CR-1063, June 1968.
-
(1968)
An Analysis of a Chemically Reacting Boundary Layer and Charring Ablator: Part IV A Unified Approximation for Mixture Transport Properties for Multi-Component Boundary Layer Calculations
-
-
Bartlett, E.P.1
Kendall, R.M.2
Rindal, R.A.3
-
13
-
-
0003581172
-
-
Accurex Corporation, Mountain View, CA
-
Kendall, R. M., Rindal, R. A., and Bartlett, E. P., "Users Manual, CMA87S, Aerotherm Charring Material Thermal Response and Ablation Program," Accurex Corporation, Mountain View, CA 1987.
-
(1987)
Users Manual, CMA87S, Aerotherm Charring Material Thermal Response and Ablation Program
-
-
Kendall, R.M.1
Rindal, R.A.2
Bartlett, E.P.3
-
15
-
-
85086811671
-
-
Gokcen, T., Skokova, K., Balboni, J.A., Terrazas-Salinas, I., Bose, D., "Computational Analysis of Arc-Jet Wedge Calibration Tests in IHF 6-Inch Conical Nozzle,".
-
Computational Analysis of Arc-Jet Wedge Calibration Tests in IHF 6-Inch Conical Nozzle
-
-
Gokcen, T.1
Skokova, K.2
Balboni, J.A.3
Terrazas-Salinas, I.4
Bose, D.5
|