Studies on High Burning Rate Composite Propellant Formulations using TATB as Pressure Index Suppressant
MEHILAL, Shekhar JAWALKAR, Ramesh KURVA, Nandagopal SUNDARAMOORTHY, Ganesh DOMBE, Praveen Prakash SINGH and Bikash BHATTACHARYA
Słowa Kluczowe: composite propellant, ammonium perchlorate, TATB, pressure index suppressant
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