1Oberle, W., and White, K. 1997. The Application of Electrothermal-Chemical (ETC) Propulsion Concepts to Reduce Propelling Charge Temperature Sensitivity. ARL-TR-1509, U.S. Army Ballistic Research Laboratory, Aberdeen Proving Ground, MD 21005-5066.
2Clifford, W. 1982. Temperature Sensitivity of Aircraft Cannon Propellants. AFATL-TR-82-72.
3Clifford, W., and Bertram, K. 1982. Ballistic criteria for Propellant Grain Fracture in the GAU-8/A 30 MM Gun. AFATL-TR-82-21.
4Jeunieau, L., Lefebvre, M. H., Papy, A., Pirlot, M. C. Guillaume, P., and Reynaud, C. 2002. "Closed Vessel Test: Influence of the Ignition Method on the Combustion Rate." In 33th International Annual Conference of ICT,Karlsruhe.
5STANAG 4115. 1997. Definition and Determination of Ballistic Properties of Gun Propellants. North Atlantic Council.
6Jeunieau, L., Lefebvre, M. H., Papy, A., Pirlot, M. C., Guillaume, P., and Reynaud, C. 2003. "Spherical Deterred Propellant: Influence of the Concentration Gradient on the Burning Rate Calculation." In 34th International Annual Conference of lCT, Karlsruhe.
7Jeunieau, L., Lefebvre, M. H., and Guillaume, P. 2007. "Ballistic Stability of a Spherical Propellant: Comparison with a Flattened Spherical Propellant." Central EuropeanJournal of Energetic Materials 4 (I-2): 31-44.
8EN 13631-4. 2003. Explosives for Civil Uses-High Explosives-Part 4: Determination of Sensitiveness to lmpact of Explosives. European Committee for Standardization, 2002.
9STANAG 4489. 1999. Explosives, lmpact Sensitivity Tests. NATO Standardization Agreement.
10Jeunieau, L., Lefebvre, M. H., Guillaume, P., Wilker, S., Chevalier, S., and Eibl, S. 2004. "Stability Analyses of Rolled Ball Propellants, Part II-Ballistic Stability." In 35th International Annual Conference of lCT, Karlsruhe, pp. 15-28.
