Numerical Study on Response Characteristics of Solid Rocket Pintle Motor

Autor: Yi Hua Xu, Hai Jun Sun, Jeevan Sapkota

Publikováno v: Journal of Aerospace Technology and Management v.11 2019
Journal of Aerospace Technology and Management
Departamento de Ciência e Tecnologia Aeroespacial (DCTA)
instacron:DCTA
Journal of Aerospace Technology and Management, Vol 11, Iss 1, Pp 3419-3419 (2019)

Pintle technology is currently a versatile technology used in a solid rocket motor (SRM) to control the desired thrust by changing the nozzle throat area, while effectively controlling the chamber pressure at the same time. The sudden movement of the

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