1. and “Analyses of Processing Variables in Propellant Burn Rate and Modulus—[1] Mixing Times,” Proceedings of the 13th International Symposium on Space Technology and Science, Tokyo, 1982, pp. 117-124.
2. and “Space Shuttle Solid Rocket Motor Reproducibility and the Apparent Influence of Propellant Processing Characteristics on Trace Shape,” AIAA, 89-2310, 25th Joìnt Propulsion Conference, Monterey, CA, 1989.
3. and “The Effect of Oxidizer Particle Size Distribution on the Steady and Nonsteady Combustion of Composite Propellants,” Technical Report AFRPL-TR-78-17, Air Force Rocket Propulsion Laboratory, Jun 1978.