ionel Borne 724 Solid-Liquid Adhesion Energies of Composite Propellant Components Determinedb yS olution Calorimetry Michael M. Nardai, ManfredA .B ohn 728 Modeling, Simulation and Characterization of Complex Shaped Solid PropellantC ombustion Sebastian Wurster 736 Evaluationo ft he James Initiation Criterion in the 21 mm and 50 mm PMMAG ap Te st Sebastian Wurster 749 R Re ev vi ie ew w The cover picture shows as even-hole propellant of type NK 1074 that was aged for 36 years at 35 8C, 40 8C, 45 8C, and 50 8C. The 50 8Cs ample shows serious decomposition with completel oss of the grain structure. The other samples do not show alarge differenceinoptical appearance. Periodic mass loss oscillationsf or A5020 propellant can be observed over the temperature range of 30 8Ct o7 08Cw ithout temperature dependence. Additionally the Arrheniusp lot for decompositionv ia mass loss for an A5200 propellant is shown. It shows av ery good correlation of the formal and the simplified model applied in mass loss analysis. Details are discussed in the article by Moritz Heil et al. on page7 06.