1. Ur Rahman Khan A (2011) Methodology for integrated thermo structural analysis of solid rocket nozzle with ablative composite liners. In: ISAMPE national conference on composites—INCCOM 10, November 18–19, 2011. Research and Development Establishment (Engineers), Pune
2. Shih PK, Prunty J, Mueller RN (1988) Thermo structural concepts for hypervelocity vehicles. AIAA, 88-2295, pp 651–658
3. Coulbert CD (1963) Selecting a thrust chamber cooling technique for spacecraft rocket engines. AlAA Summer Meeting, California
4. Stetson JR, Miyazawa ET, Groener LS, Legendre PJ, Capt. Bohlen JW (1979) Experimental evaluation of thermostructural shear stresses on re-entry performance of carbon-carbon nose tips. AlAA
5. Milos FS, Squire TH (1999) Thermostructural analysis of X-34 wing leading-edge tile thermal protection system. J Spacecr Rockets 36(2):189–198