[1]
Prabu G, A.S. , Raj, V. , Khan, I. and Balloli, A. 2019. IGNITION SYSTEM ON SOLID ROCKET MOTOR FOR 10000 N THRUST, USING HTPB AS AN FUEL AND OXIDISER. International Journal of Technical Innovation in Modern Engineering & Science. 5, 5 (May 2019), 779–783.