Follow
Dinesh Prabhu
Dinesh Prabhu
Verified email at nasa.gov
Title
Cited by
Cited by
Year
FIRE II calculations for hypersonic nonequilibrium aerothermodynamics code verification: DPLR, LAURA, and US3D
D Hash, J Olejniczak, M Wright, D Prabhu, M Pulsonetti, B Hollis, P Gnoffo, ...
45th AIAA Aerospace Sciences Meeting and Exhibit, 605, 2007
1362007
Absolute radiation measurement in venus and mars entry conditions
BA Cruden, D Prabhu, R Martinez
Journal of Spacecraft and Rockets 49 (6), 1069-1079, 2012
1122012
Adaptive deployable entry and placement technology (ADEPT): a feasibility study for human missions to Mars
E Venkatapathy, K Hamm, I Fernandez, J Arnold, D Kinney, B Laub, ...
21st AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar …, 2011
1122011
Radiation modeling for the reentry of the Stardust sample return capsule
Y Liu, D Prabhu, KA Trumble, D Saunders, P Jenniskens
Journal of Spacecraft and Rockets 47 (5), 741-752, 2010
722010
Uncertainty assessment of hypersonic aerothermodynamics prediction capability
D Bose, JL Brown, DK Prabhu, P Gnoffo, CO Johnston, B Hollis
Journal of Spacecraft and Rockets 50 (1), 12-18, 2013
692013
Analysis and model validation of shock layer radiation in air
D Bose, E McCorkle, C Thompson, D Bogdanoff, D Prabhu, G Allen, ...
46th AIAA Aerospace Sciences Meeting and Exhibit, 1246, 2008
672008
Investigation of nonequilibrium radiation for Mars entry
A Brandis, C Johnston, M Panesi, B Cruden, D Prabhu, D Bose
51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and …, 2013
642013
Transition experiments on blunt bodies with distributed roughness in hypersonic free flight
DC Reda, MC Wilder, DW Bogdanoff, DK Prabhu
Journal of Spacecraft and Rockets 45 (2), 210-215, 2008
612008
An analysis of the radiative heating environment for aerocapture at Titan
J Olejniczak, D Prabhu, M Wright, N Takashima, B Hollis, K Sutton, E Zoby
39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 4953, 2003
602003
Temperature constraints at the sharp leading edge of a crew transfer vehicle
D Kontinos, K Gee, D Prabbu
35th AIAA thermophysics conference, 2886, 2001
592001
Analysis of Apollo command module afterbody heating Part I: AS-202
MJ Wright, DK Prabhu, ER Martinez
Journal of Thermophysics and heat Transfer 20 (1), 16-30, 2006
572006
Arcjet testing in shear environment for Mars Science Laboratory thermal protection system
DM Driver, JE Carballo, R Beck, D Prabhu, JA Santos, A Cassell, ...
Journal of Spacecraft and Rockets 51 (4), 1151-1166, 2014
562014
Assessment of laminar, convective aeroheating prediction uncertainties for Mars-entry vehicles
BR Hollis, DK Prabhu
Journal of Spacecraft and Rockets 50 (1), 56-68, 2013
562013
Aerocapture systems analysis for a Neptune Mission
MK Lockwood, KT Edquist, BR Starr, BR Hollis, GA Hrinda, RW Bailey, ...
522006
Current grid-generation strategies and future requirements in hypersonic vehicle design, analysis and testing
P Papadopoulos, E Venkatapathy, D Prabhu, MP Loomis, D Olynick
Applied Mathematical Modelling 23 (9), 705-735, 1999
521999
Conformal phenolic impregnated carbon ablator arcjet testing, ablation, and thermal response
FS Milos, MJ Gasch, DK Prabhu
Journal of Spacecraft and Rockets 52 (3), 804-812, 2015
502015
Analysis of air radiation measurements obtained in the EAST and X2 shocktube facilities
A Brandis, B Cruden, D Prabhu, D Bose, M McGilvray, R Morgan, ...
10th AIAA/ASME Joint Thermophysics and Heat Transfer Conference, 4510, 2010
492010
Equilibrium Radiative Heating from to for Earth Atmospheric Entry
AM Brandis, CO Johnston, BA Cruden, DK Prabhu
Journal of Thermophysics and Heat Transfer 31 (1), 178-192, 2017
482017
Validation of CO 4th positive radiation for Mars entry
AM Brandis, CO Johnston, BA Cruden, DK Prabhu, AA Wray, Y Liu, ...
Journal of Quantitative Spectroscopy and Radiative Transfer 121, 91-104, 2013
462013
Transition experiments on blunt bodies with isolated roughness elements in hypersonic flight
DC Reda, MC Wilder, DK Prabhu
Journal of Spacecraft and Rockets 47 (5), 828-835, 2010
452010
The system can't perform the operation now. Try again later.
Articles 1–20