Uncertainty Analysis of Radiative Heating Predictions for Titan Entry

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

Reference55 articles.

1. Committee on the Planetary Science Decadal Survey, “Vision and Voyages for Planetary Science in the Decade 2013-2022,” National Research Council of the National Academies, TR, Washington, D.C. 2011, http://solarsystem.nasa.gov/docs/Vision_and_Voyages-FINAL.pdf.

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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