论文信息 - Arc Jet Testing in a Shear Environment for Mars Science Laboratory Thermal Protection System - 字舞流文

Arc Jet Testing in a Shear Environment for Mars Science Laboratory Thermal Protection System

David M. Driver | Dinesh K. Prabhu | William Willcockson | Eric Slimko | Alan Cassell | Robin Beck | Kristina Skokova | Chun Y. Tang | Helen Hwang | Jarvis Songer | E. Slimko | D. Driver | W. Willcockson | A. Cassell | D. Prabhu | Helen H. Hwang | Robin Beck | K. Skokova | Chun Tang | J Carballo | Jose Santos | J. Songer | J. Carballo | Jose Santos

[1] Karl T. Edquist,et al. Aerothermodynamic Design of the Mars Science Laboratory Heatshield , 2009 .

[2] Frank S. Milos,et al. Ablation and Thermal Response Program for Spacecraft Heatshield Analysis , 1999 .

[3] Daniel J. Rasky,et al. Phenolic Impregnated Carbon Ablators (PICA) as Thermal Protection Systems for Discovery Missions , 1997 .

[4] G. Candler,et al. Data-Parallel Line Relaxation Method for the Navier -Stokes Equations , 1998 .

[5] W. Winovich,et al. The 60-MW Shuttle interaction heating facility , 1979 .

[6] Bernard Laub,et al. Development of a High-Fidelity Thermal/Ablation Response Model for SLA-561V , 2009 .

[7] N. R. Keltner,et al. Transient response of circular foil heat‐flux gauges to radiative fluxes , 1975 .

[8] E. Strauss. Superlight ablative systems for Mars lander thermal protection. , 1967 .

[9] V. A. Petrov,et al. Spectral emissivity and absorption coefficient of silica glass at extremely high temperatures in the semitransparent region , 1979 .