%0 Journal Article %A Ramachandran, Lalitha %A Krishnan, T. E. %A Kurian, A. J. %A Rao, S. Somesware %A Ninan, K. N. %D 1994 %I Begell House %N 1-6 %P 659-661 %R 10.1615/IntJEnergeticMaterialsChemProp.v3.i1-6.640 %T TEMPERATURE SENSITIVITY STUDIES ON NITRAMINE-BASED PROPELLANT %U https://www.dl.begellhouse.com/journals/17bbb47e377ce023,15629a1604e1b6b4,7adf54dd01fdc08b.html %V 3 %X 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. %8 1994-01-01