“…To evaluate the potential of the compounds as a possible future component of solid rocket propellants, we calculated the performances of reported compounds using the recently described Klapötke and Suceska method 39 of specific impulse with various composite mixtures containing 10% glycidyl azide polymer (GAP), 15% nitroglycerin (NG), 18% aluminum, a variable percentage (57%) of the oxidizer ammonium perchlorate (AP) and an energetic filler to attain the oxygen balance −33% with respect to CO 2 , which corresponds to modern propellant formulation (70% AP, 16% Al, 12% HTPB and 2% epoxy) with practical applications. Using this method, the calculated specific impulses (with the EXPLO-5 (v 6.02.02) software) of compounds 2 , 3 , 4 , 9 , and 10 are 268.3, 271.7, 270.3, 268, and 272 s, respectively (detailed calculation (ESI, Table S10†), which offers better impulse values than a modern propellant formulation (70% AP, 16% Al, 12% HTPB and 2% epoxy) with a calculated specific impulse of 264 s. 40…”