Numerical Study on Response Characteristics of Solid Rocket Pintle Motor
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 pintle can induce rapid changes in the flow field...
| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
| Published: |
Departamento de Ciência e Tecnologia Aeroespacial
2019-08-01
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| Series: | Journal of Aerospace Technology and Management |
| Subjects: | |
| Online Access: | http://www.scielo.br/pdf/jatm/v11/2175-9146-jatm-11-e3419.pdf |