Transient aero-thermal mapping of passive Thermal Protection system for nose-cap of Reusable Hypersonic Vehicle

Author:

Mahulikar Shripad P.,Khurana Shashank,Dungarwal Ritesh,Shevakari Sushil G.,Subramanian Jayakumar,Gujarathi Amit V.

Publisher

Springer Science and Business Media LLC

Subject

Space and Planetary Science,Aerospace Engineering

Reference35 articles.

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2. FOLEY, T.M. “Big Hopes for Small Launchers,” Aerospace America, Vol. 33, No. 7, May 1995, pp. 28–34.

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4. FREEMAN, D. C., TALAY, T. A., and AUSTIN, R. E. “Single-Stage-to-Orbit Meeting the Challenge,” Acta Astronautica, Vol. 38, Nos. 4–8, February 1996, pp. 323–331.

5. TRAN, H. K., RASKY, D. J., and ESFAHANI, L. “Thermal Response and Ablation Characteristics of Lightweight Ceramic Ablators,” Journal of Spacecraft and Rockets, Vol. 31, No. 6, November–December 1994, pp. 993–998.

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