Preliminary Design Approach for Sub-Scale Rocket Motor Thrust Stand
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Publisher
Springer Nature Singapore
Link
https://link.springer.com/content/pdf/10.1007/978-981-19-1388-4_1
Reference9 articles.
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5. Shukla H, Nandan GRS, Shukla P, Kumar V, Varma M (2017) Ignition and combustion characteristics of a micro-electromechanical system (MEMS) pyrotechnic thruster for micro propulsion applications. Int J Energet Mater Chem Propuls 16(2)
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1. Energetic material characterization and ignition study of MEMS based micro-thruster for multi spacecrafts missions;FirePhysChem;2023-08
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