FEASIBILITY DEMONSTRATION OF A TRANSPIRATION COOLED NOZZLE SYSTEM (2006)
Smith, K. J., Poulos, E. N., Steigerwald, E. A., Lally, F., Peck, J. V., Pappas, C.
The use of transpiration cooling for advanced solid propellant application is described. The mechanism used for demonstration purposes consisted of a porous tungsten insert cooled by anhydrous...
THRUST CHAMBER MATERIALS AND DESIGN CONCEPTS EVALUATION (2005)
Parks, Edgar G., Jr., Crump, D. N., Poulos, E. N., Pearson, J. B., Smith, K. J.
A program was conducted to investigate and evaluate new and unique designs of non-regenerative combustion chambers and nozzles using new materials or new techniques for applying the best materials....