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Journal:Journal of Space Technology, 2017, Volume 17, Issue No 1

Author(s): D. Noman, Irfan Mahmood Khan, M. Zeeshan Siddiqui, M. Shahzad, Bilal Ahmed

Keyword(s): Positive expulsion devices, Heat Effected Zone, secondary propulsion system, Elastomeric diaphragm, Thermal integrity, FKM