[1] P. Ducasse, “Rocket altitude test facilities register,” ADVISORY GROUP FOR AEROSPACE RESEARCH AND DEVELOPMENT NEUILLY-SUR-SEINE (FRANCE), 1987.
[2] J. N. Sivo, C. L. Meyer, and D. J. Peters, Experimental Evaluation of Rocket Exhaust Diffusers for Altitude Simulation. National Aeronautics and Space Administration, 1960.
[3] B. H. Park, J. Lim, S. Park, J. H. Lee, and W.-S. Yoon, “Design and Analysis of a Second-Throat Exhaust Diffuser for Altitude Simulation,” Journal of Propulsion and Power, vol. 28, no. 5, pp. 1091–1104, Sep. 2012, doi: 10.2514/1.B34342.
[4] B. H. Park, J. H. Lee, and W. Yoon, “Studies on the starting transient of a straight cylindrical supersonic exhaust diffuser: Effects of diffuser length and pre-evacuation state,” International Journal of Heat and Fluid Flow, vol. 29, no. 5, pp. 1369–1379, Oct. 2008, doi: 10.1016/j.ijheatfluidflow.2008.04.006.
[5] N. Fouladi, “Numerical investigation of flow transient phase of motor burnout in an altitude test simulator,” Modares Mechanical Engineering, vol. 18, no. 7, pp. 10–19, Nov. 2018.
[6] K. Annamalai, K. Visvanathan, V. Sriramulu, and K. A. Bhaskaran, “Evaluation of the performance of supersonic exhaust diffuser using scaled down models,” Experimental Thermal and Fluid Science, p. 13, 1998.
[7] J. Lim, B. H. Park, W. Yoon, and Y. Lee, “Parametric Investigation on the Essential Flow Factors Commanding Steady Operations of the Second Throat Exhaust Diffuser,” in 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Hartford, CT: American Institute of Aeronautics and Astronautics, Jul. 2008. doi: 10.2514/6.2008-4784.
[8] H.-G. Sung, H.-W. Yeom, S. Yoon, S.-J. Kim, and J. Kim, “Investigation of Rocket Exhaust Diffusers for Altitude Simulation,” Journal of Propulsion and Power, vol. 26, no. 2, pp. 240–247, Mar. 2010, doi: 10.2514/1.46226.
[9] R. Arun Kumar and G. Rajesh, “Flow transients in un-started and started modes of vacuum ejector operation,” Physics of Fluids, vol. 28, no. 5, p. 056105, May 2016, doi: 10.1063/1.4948959.
[10] R. Arun Kumar and G. Rajesh, “Physics of vacuum generation in zero-secondary flow ejectors,” Physics of Fluids, vol. 30, no. 6, p. 066102, Jun. 2018, doi: 10.1063/1.5030073.
[11] N. Fouladi, M. Farahani, and A. R. Mirbabaei, “Performance evaluation of a second throat exhaust diffuser with a thrust optimized parabolic nozzle,” Aerospace Science and Technology, vol. 94, p. 105406, Nov. 2019, doi: 10.1016/j.ast.2019.105406.
[12] N. Fouladi and M. Farahani, “Numerical investigation of second throat exhaust diffuser performance with thrust optimized parabolic nozzles,” Aerospace Science and Technology, vol. 105, p. 106020, Oct. 2020, doi: 10.1016/j.ast.2020.106020.
[13] N. Fouladi, “Numerical investigation of back flow arrester effect on altitude test simulator starting performance,” Modares Mechanical Engineering, vol. 17, no. 7, pp. 185–196, 2017.
[14] N. Fouladi, A. Mohamadi, and H. Rezaei, “Numerical design and analysis of supersonic exhaust diffuser in altitude test simulator,” Modares Mechanical Engineering, vol. 16, no. 8, pp. 159–168, Oct. 2016.
[15] H. L. Merryman and R. M. Brooksbank, “Quality Assurance Test of a Thiokol Chemical Corporation TE-M-364-3 Solid-Propellant Rocket Motor Tested in the Spin Mode at Simulated Altitude Conditions,” ARO INC ARNOLD AFS TN, 1970.
[16] R. Manikanda Kumaran, K. Vivekanand, T. Sundararajan, S. Balasubramanian, and D. Raja Manohar, “Analysis of Diffuser and Ejector Performance in a High Altitude Test Facility,” in 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Denver, Colorado: American Institute of Aeronautics and Astronautics, Aug. 2009. doi: 10.2514/6.2009-5008.
[17] E. Mohammadi, N. Fouladi, and A. Madadi, “Design and Analysis of Gas Ejector in High Altitude Test Facility,” Amirkabir Journal of Mechanical Engineering, vol. 52, no. 11, pp. 3015–3032, 2019.
