Uncertainty Analysis of Radiative Heating Predictions for Titan Entry-Reference-Cited by-同舟云学术

Uncertainty Analysis of Radiative Heating Predictions for Titan Entry

Published:2016-04 Issue:2 Volume:30 Page:438-451
ISSN:0887-8722
Container-title:Journal of Thermophysics and Heat Transfer
language:en
Short-container-title:Journal of Thermophysics and Heat Transfer

Author:

West Thomas K.¹,Brune Andrew J.¹,Hosder Serhat¹,Johnston Christopher O.²

Affiliation:

1. Missouri University of Science and Technology, Rolla, Missouri 65409

2. NASA Langley Research Center, Hampton, Virginia 23681

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Condensed Matter Physics,Aerospace Engineering,Space and Planetary Science,Fluid Flow and Transfer Processes,Mechanical Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.T4620

Reference55 articles.

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2. ZangT. A.Dwyer-CiancoloA. M.KinneyD. J.HowardA. R.ChenG. T.IvanovM. C.SostaricR. R.WesthelleM. C. “Overview of the NASA Entry, Descent, and Landing Systems Analysis Studies for Large Robotic-Class Missions,” AIAA Paper 2010-8649, Aug. 2010.

3. Dwyer-CiancoloA. M.DavisJ. L.ShidnerJ. D.PowellR. W. “Entry, Descent, and Landing Systems Analysis: Exploration Class Simulation Overview and Results,” AIAA Paper 2010-7970, Aug. 2010.

4. Dwyer-CiancoloA. M.DavisJ. L.EngelundW. C.KomarD. R.QueenE. M.SamarehJ. A.WayD. W.ZangT. A. “Entry, Descent, and Landing Systems Analysis Study: Phase 2 Report on Exploration Feed-Forward Systems,” NASA TR-TM-217055, Feb. 2011.

5. Flexible Ablative Thermal Protection Sizing on Inflatable Aerodynamic Decelerator for Human Mars Entry Descent and Landing

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