RT Journal Article ID 7adf54dd01fdc08b A1 Ramachandran, Lalitha A1 Krishnan, T. E. A1 Kurian, A. J. A1 Rao, S. Somesware A1 Ninan, K. N. T1 TEMPERATURE SENSITIVITY STUDIES ON NITRAMINE-BASED PROPELLANT JF International Journal of Energetic Materials and Chemical Propulsion JO IJEMCP YR 1994 FD 1994-01-01 VO 3 IS 1-6 SP 659 OP 661 AB Rocket motors stored in ambient conditions experience the variations in environmental temperature. This can result in dispersion of the burning rate of the grain due to the temperature sensitivity characteristic of the propellant formulation. In order to study this on a nitramine-based propellant, experiments are carried out at both strand level and motor level. The results show that strand level investigation is as good as actual motor tests. PB Begell House LK https://www.dl.begellhouse.com/journals/17bbb47e377ce023,15629a1604e1b6b4,7adf54dd01fdc08b.html