1. V.N. Berezhnoy, Activities in support of ground-base development testing of Liquid Rocket Engines (LRE) incorporating high-expansion ratio nozzles, Abstracts of the 14th International Conference “Aviation and Cosmonautics — 2015”, 2015, Moscow, MAI, 2015. P. 99–100.
2. P. Pempie and H. Vernin, Liquid rocket engine test plan comparison, in: 37th Joint Propulsion Conference and Exhibition, AIAA Paper, 2001, No. 2001-3256.
3. J.R. Bullock, M. Popp, and J. Santiago, Program status of the pratt & whitney RL60 engine, in: 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibition, AIAA Paper, 2002, No. 2002-3587.
4. J. Steelant, M. Marini, G. Pezella, B. Reimann, S.L. Chernyshev, A.A. Gubanov, V.A. Talyzin, N.V. Voevodenko, N.V. Kukshinov, A.N. Prokhorov, A.J. Neely, C. Kenell, D. Verstraete, and D. Buttsworth, Numerical and experimental research on the aerodynamics of high-speed passenger vehicle within the HEXAFLY-INT project, in: Proc. of the 30th Congress of the Inter. Council of the Aeronautical Sci., Daejeon, 2016, ICAS2016-0353, 2016.
5. V.Yu. Aleksandrov, N.V. Kukshinov, A.N. Prokhorov, and A.V. Rudinskiy, Analysis of the integral characterristics of HEXAFLY-INT facility module, in: Proc. of the 21th Inter. Space Planes and Hypersonic Systems and Technology Conf., Xiamen, 2017, AIAA Paper, 2017, No. 2017-2179.