1. ASTM E457-08 (2015) Standard test method for measuring heat-transfer rate using a thermal capacitance (Slug) calorimeter, ASTM International, West Conshohocken, PA, 2015. http://www.astm.org
2. Bouilly JM, Dariol L, Leleu F (2006) Ablative thermal protections for atmospheric entry. An overview of past missions and needs for future programmes. In: European Space Agency, (Special Publication) ESA SP
3. Varghese RC, Anoop P, Sundar B (2019) Heat flux estimation and TPS design of crew module for Gaganyaan Mission. VSSC Internal Report, VSSC/AHTG/PN-GY/37/2019
4. Grinstead J, Stewart D, Smith C (2005) High enthalpy test methodologies for thermal protection systems development at NASA ames research center. In: AIAA/CIRA 13th international space planes and hypersonics systems and technologies conference, vol. 2, pp. 1118–1131. American Institute of Aeronautics and Astronautics, Reston, Virigina. https://doi.org/10.2514/6.2005-3326
5. Laub B, Venkatapathy E (2004) Thermal protection system technology and facility needs for demanding future planetary missions. Eur Space Agency (Spec Publ) ESA SP 544:239–247