Mars Sample Return Orbiter

AIAA- 2001 -3068Afterbody HeatingCharacteristicsof a ProposedMars SampleReturn OrbiterThomas J. Horvath, _._,Nicholas C. Heiner,Daniella M. Olguin,F. McNeil Cheatwood andPeter A. GnoffoNASA Langley Research CenterHampton, Virginia 23681-219935th AIAA ThermophysicsConference11-14 June 2001 / Anaheim, CA

[1]  Cheatwood F. McNeil,et al.  User''s Manual for the Langley Aerothermodynamic Upwind Relaxation Algorithm (LAURA) , 1996 .

[2]  Scott A. Berry,et al.  X-38 Experimental Aerothermodynamics , 2000 .

[3]  N. Ronald Merski,et al.  Global Aeroheating Wind-Tunnel Measurements Using Improved Two-Color Phosphor Thermography Method , 1999 .

[4]  Thomas J. Horvath,et al.  Blunt body near-wake flow field at Mach 10 , 1997 .

[5]  Scott A. Berry,et al.  Shuttle Orbiter Experimental Boundary-Layer Transition Results with Isolated Roughness , 1998 .

[6]  Howard H. Hamilton,et al.  X-33 Experimental Aeroheating at Mach 6 Using Phosphor Thermography , 1999 .

[7]  Charles G. Miller,et al.  Description and calibration of the Langley Hypersonic CF4 tunnel: A facility for simulating low gamma flow as occurs for a real gas , 1985 .

[8]  A Mitcheltree Robert,et al.  Preliminary Thermal Analysis of a Mars Sample Return Earth Entry Vehicle , 2000 .

[9]  John W. Paulson,et al.  Experimental and computational analysis of the Space Shuttle Orbiter hypersonic 'pitch-up anomaly' , 1994 .

[10]  Scott A. Berry,et al.  X-34 experimental aeroheating at Mach 6 and 10 , 1998 .

[11]  R Hollis Brian.  Experimental and Computational Aerothermodynamics of a Mars Entry Vehicle , 1996 .

[12]  Merski N. Ronald.  Reduction and Analysis of Phosphor Thermography Data With the IHEAT Software Package , 1998 .

[13]  Scott A. Berry,et al.  X-33 experimental aeroheating at Mach 6 using phosphor thermography , 1999 .

[14]  P. Gnoffo.  Planetary-Entry Gas Dynamics , 1999 .

[15]  P. Gnoffo.  An upwind-biased, point-implicit relaxation algorithm for viscous, compressible perfect-gas flows , 1990 .

[16]  Scott A. Berry,et al.  X-34 Experimental Aeroheating at Mach 6 and 10 , 1998 .

[17]  R A Mitcheltree,et al.  A Passive Earth-Entry Capsule for Mars Sample Return , 1998 .

[18]  Robert D. Braun,et al.  Computation of near-wake, aerobrake flowfields , 1992 .

[19]  J. H. Thomas,et al.  Transition and Turbulence Modeling for Blunt-Body Wake Flows , 1997 .

[20]  E Glass Christopher,et al.  A 3-D Coupled CFD-DSMC Solution Method With Application to the Mars Sample Return Orbiter , 2000 .

[21]  Christopher J. Cerimele,et al.  Aeroassist vehicle requirements for a Mars Rover/Sample Return Mission , 1988 .

[22]  S. Zeiberg.  Transition correlations for hypersonic wakes , 1964 .

[23]  J. E. Pavlosky,et al.  A preliminary TPS design for MRSR - Aerobraking at Mars and at earth , 1990 .

[24]  William Wells.  Measured and predicted aerodynamic heating on a cylinder in wake of AFE configuration at incidence , 1989 .

[25]  Peter A. Gnoffo,et al.  Computational Aerothermodynamics in Aeroassist Applications , 2001 .

[26]  Gregory M. Buck,et al.  Automated thermal mapping techniques using chromatic image analysis , 1989 .