Studies on High Burning Rate Composite Propellant Formulations using TATB as Pressure Index Suppressant – Łukasiewicz-IPO

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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