[2] Hammond, W.E., Design Methodologies for Space Transportation Systems, AiAA, 2001.
[3] AESTUS: Upper Stage Engine manual ASTRIUM Space Transportation, 2015.
[4] Ley, W., Klaus W. and Willi H., eds. Handbook of Space Technology, Vol. 22. John Wiley & Sons, 2009.
[5] Bruno, C, and Accettura, A.G., Advanced Propulsion Systems and Technologies, Today to 2020. Vol. 223, Amer Inst of Aeronautics &, 2008.
[6] Moon, Yongjun, et al. “Design Specifications Of H 2O2/Kerosene Bipropellant Rocket System For Space Missions,” Aerospace Science and Technology, Vol. 33, No. 1 , 2014, pp. 118-121.
[7] Sutton, George P., and Oscar B., Rocket Propulsion Elements, John Wiley & Sons, 2016.
[8] Humble, R.W., Gary N. Henry, and Wiley J. Larson, eds. Space Propulsion Analysis and Design. Vol. 1. New York: McGraw-Hill, 1995.
[9] Adami, Amirhossein, Mortazavi, M. and Nosratollahi M., "A New Approach in Multidisciplinary Design Optimization of Upper-Stages Using Combined Framework." Acta Astronautica, Vol. 114, 2015, pp.174-183.
[10]Tajmar, M., Advanced Space Propulsion Systems, Springer Science & Business Media, 2012.
[11]Fatehi, M., Nosratollahi, M., Adami, A.H. and Taherzadeh, S.M,. “Designing Space Cold Gas Propulsion System using Three Methods: Genetic Algorithms, Simulated Annealing and Particle Swarm,” International Journal of Computer Applications, Vol. 118, No. 22, 2015.
[12]Fortescue, P., Swinerd, G. and Stark, J. eds. Spacecraft systems engineering, John Wiley & Sons, 2011.
[13]Adami, A.H. and et al. “Multidisciplinary Design Optimization and Analysis of Hydrazine Monopropellant Propulsion System. ”International Journal of Aerospace Engineering 2015.
[14]Huzel, D.K., and H. Huang, D., Modern Engineering for Design of Liquid-Propellant Rocket Engines, AiAA, Vol. 147, 1992.
[15] Schmidt, E.W., Hydrazine and Its Derivatives, Preparation, Properties, Applications,2nd ed., John Wiley & Sons, New York, 2001.
[16] Sanford Gordon, Bonnie J. McBride, Computer Program for Calculation of Complex Chemical Equilibrium Compositions and Applications, NASA, Lewis Research Center, Cleveland, Ohio, 1994, Technical Report.
[17] Erichsen, P., “Spacecraft Propulsion with System Impulse Performance Analysis,” 2011.
[18] Taylor, Travis S., Introduction to Rocket Science and Engineering. CRC Press, 2017.
[19] Global Optimization Toolbox, Matlab User guide, 2019.
[20] Available, [On Line]: http://www.space-propulsion.com/launcher-propulsion/rocket-engines/aestus-rocket-engine.html
[21] Lacoste, M. and et al. “Carbon/Carbon Extendible Nozzles,” Acta astronautica, Vol. 50, No. 6 2002, pp.357-367.
[22] Potapov, A., Shtefan, Y. and Lichman, E., “Research of Material for Uncooled Nozzle Extensions of Liquid Rocket Engines,” Acta Astronautica, Vol. 64, No.1, 2009, pp. 22-27.
[23] Valentine, P.G., Lee, R. Allen, P. Gradl and et al., “Upper Stage Engine Composite Nozzle Extensions,” Conference: 53rd AIAA/SAE/ASEE Joint Propulsion Conference, 2015.
[24] Propellant Tank Lineup IHI Aero Space Data Sheet, IHI Aerospace Co., Ltd, in Available, [On Line]: https://www.ihi.co.jp/ia/en/products/space/ tanks/index.html
[25] Available, [On Line]: http://www.psi-pci.com/ Data_Sheets1_main.htm
[26] Available, [On Line]: Aerojet Propellant Tank Data Sheet.
[27] Muhalim, N. M. F. and Krishnan, S., “Design of Nitrogen-Tetroxide/Monomethyl-Hydrazine Thruster for Upper Stage Application,” Published 2013.
[28] Tam, Walter H. and et al., “Low Cost Derivative Tanks for Spacecraft and Launch Vehicles,” AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 35Th, Los Angeles, CA. 1999.
[29] Muhalim, N.M.F. B., and Subramaniam Krishnan. “Design of Nitrogen-Tetroxide/ Monomethyl-Hydrazine Thruster for Upper Stage Application,” Published 2013.
[30] Available: [On Line],
http://www.space-propulsion.com/launcher-propulsion/rocket- engines/vinci-rocket-engine.html
[31] Mouritz, A.P., Introduction to Aerospace Materials, Elsevier; 2012 May 23.
[32] Nieroski, John S., and Edward I. Friedland. “Liquid Rocket Engine Cost Estimating Relationships,” AIAA Paper, 1965, 65-533.
[33] Frank, C., Pinon, O., Tyl, C. and Mavris, D.N., “New Design Framework For Performance, Weight, and Life-Cycle Cost Estimation of Rocket Engines,” 6th European Conference for Aerospace Sciences - EUCASS At: Krakow, Poland 2015.
[34] Available, [On line]: http://www.metalprices.com
[35] Shama Rao N., Simha T.G.A., Rao K.P., Ravi Kumar G. V. V., Carbon Composites are Becoming Competitive and Cost Effective (Infosys), 2015
[36] Available, [On line]: https://www. midweststeelsupply.com.
[37] Defense Logistics Agency, “Aerospace Energy Standard Prices for DOD Customers Effective 1 Oct 2015,” tech. rep, DLA, 2015.
[38] Ventura, Mark. The Lowest Cost Rocket Propulsion System, 42nd AIAA/ASME/SAE/ ASEE Joint Propulsion Conference & Exhibit. 2006.
