Equilibrium Emissivity Calculations for a Hydrogen Plasma at Temperatures Up to 10,000 0 K
Re-Entry Physics. Volume III. Interaction of Vehicles in Early Re-Entry Environment. Chapters 1-5
Study of Electrical Breakdown Conditions in the Aerodynamic Flow Field of a Hypersonic Vehicle
Performance Study of a Repetitively Pulsed Two-Stage Plasma Propulsion Engine Final Report
Report on the Fourth International Symposium on Rarefied Gas Dynamics