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...
| প্রধান লেখক: | , , |
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| বিন্যাস: | প্রবন্ধ |
| ভাষা: | English |
| প্রকাশিত: |
Instituto de Aeronáutica e Espaço (IAE)
2019-08-01
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| মালা: | Journal of Aerospace Technology and Management |
| বিষয়গুলি: | |
| অনলাইন ব্যবহার করুন: | http://www.scielo.br/pdf/jatm/v11/2175-9146-jatm-11-e3419.pdf |