Author:
Kumar Chandan,Prakash Akshay
Publisher
Springer Nature Singapore
Reference11 articles.
1. Johnson Joshua E, Starkey Ryan P, Lewis Mark J (2007) Aerothermodynamic optimization of reentry heat shield shapes for a crew exploration vehicle. J Spacecr Rockets 44(4):849–859. https://doi.org/10.2514/1.27219
2. Niehaus W (1963) Heat shield concept and material for reentry vehicles. In: Defence Documentation Centre, Cameron Station, Alexandria, Virginia. http://apps.dtic.mil/sti/citations/AD0439449
3. Curry DM (1965) An analysis of a charring ablation thermal protection system. In: NASA technical note NASA TN D-3150. http://ntrs.nasa.gov/citations/19660003941
4. Balakrishnan A, Nicolet W, Sandhu S (1979) Galileo probe thermal protection: entry heating environments and spallation experiment design. In: NASA contractor report-152334. http://ntrs.nasa.gov/citations/19800005927
5. Mazzaracchio A, Marchetti M (2010) A probabilistic sizing tool and Monte Carlo analysis for entry vehicle ablative thermal protection systems. Acta Astronautica 66(5):821–835. https://doi.org/10.1016/j.actaastro.2009.08.033