1. Ares I–X Flight Test Vehicle similitude to the Ares I Crew Launch Vehicle
2. Comprehensive analysis and estimation system on thermal environment, heat protection and thermal structure of spacecraft
3. Wang, X. Y., Yuko, J., and Motil, B. "Ascent heating thermal analysis on the spacecraft adaptor (SA) fairings and the interfacewith thecrew launch vehicle(CLV)",NASATM-2009-215474,2009.
4. Estruch, D. "Hypersonic Interference Aerothermodynamics", PhD Thesis,Aerospace Sciences Department, Cranfield University,Cranfield,Bedford,UK,2009.