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...