[1] Woodberry RHF (1974) Solid rocket thrust vector control. NASA SP-8114 4-17.
[2] Anon, Final report-development and demonstration of an omni axial flexibleseal movable nozzle for thrust vecotor control.thiokol chemical crop.1967
[3] RamMohan V (2012) Design modeling and experimental validation of typical flex bearing joint of rocket motor nozzle. PHD thesis.
[4] Bapi Raju V, Balakrishna Murthy V, Swetha Srinivas J (2013) Non–linear analysis of composite beam. IJAMM&C 3.
[5] Eswara Kumar A, balakrishna Murthy V, chandra Mohan,effect of shim percentage on non-linear static behavior of flex seal of rocket nozzle.Material today:proceedings 2,pp.1427-1434, 2015.
[6] Prakash D.a, Balakrishna Murthy V.b, Effect of Material Mismatch on Static behavior of Flex Seal, Materials Today: Proceedings 4, pp 2290–2297, 2017.
[7] Xiaoguang Zhang, Yu Liu, and Junxue Ren, Nonlinear finite element analysis of the SRM Flexible Joint, AIAA, 2012.
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