Simulation and Parametric Analysis of Thrust Reverser System in Solid Fuel Engines
Each missile has a payload section and an engine section. In the path of the missile, there is a time when the mission of the engine section is over and after that the engine will not play an effective role and will be as extra weight and consequently reduced range or factor for easy detection of th...
| Main Authors: | , |
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| Format: | Article |
| Language: | fas |
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Aerospace Research Institute
2023-05-01
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| Series: | فصلنامه علوم و فناوری فضایی |
| Subjects: | |
| Online Access: | https://jsst.ias.ir/article_166663_627da690b779700e50592326fef91e63.pdf |