Ballistic re-entry vehicle dispersion due to precession stoppage von Lin, T. C, Grabowsky, W. R, Yelmgren, K. E, Landa, M

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Use of radio frequency bridge for re-entry plasma diagnostics von FUHS, A. E, GRABOWSKY, W. R, GIBB, O. L

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Performance of a 500-kjoule MHD wind tunnel von GRABOWSKY, W. R., DURRAN, D. A., MIRELS, H.

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The search for optimum configurations for re-entry vehicles von Lin, Tony C, Grabowsky, Wallis R, Yelmgren, Kevin E

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Electron-magnetic-field interactions in the electron bombardment heated thruster von STARNER, K. E, GRABOWSKY, W. R

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Electron bombardment heating for electrothermal propulsion von STARNER, K. E, GRABOWSKY, W. R

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Electrode feed system for segmented electrode MHD accelerator von DURRAN, D. A, GRABOWSKY, W. R

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Hot-shot gas source for pulsed MHD ACCELERATOR von GRABOWSKY, W. R, DURBAN, D. A, SPENCER, D. J

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BASIC RESEARCH PROGRAM. RAIL GUN von GRABOWSKY, W R

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ENERGY CONVERSION PROGRAM. MAGNETOHYDRODYNAMIC GENERATOR von GRABOWSKY,W R

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GENERAL RESEARCH. ELECTRON BOMBARDMENT HEATING FOR ELECTROTHERMAL PROPULSION von Starner,K E, Grabowsky,W R

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HIGH TEMPERATURE ARC STUDIES von GRABOWSKY,W R, Spencer,D J

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Gauge for Measuring Impulsive Pressure in a Container Subjected to Large, Time‐Varying Applied Voltages von Grabowsky, W. R., Durran, D. A.

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USE OF RF BRIDGE FOR REENTRY PLASMA DIAGNOSTICS von Fuhs, A E, Gibb, O L, Grabowsky, W R

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MHD WIND TUNNEL PROGRAM von Durran,D A, Grabowsky,W R, Spencer,D J

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DOUBLE SHOCK TUBE METHOD FOR SIMULTANEOUS DETERMINATION OF HIGH PRESSURE AND TEMPERATURE OF AN ENCLOSED GAS von Grabowsky,W R, Lam,L Y, Durran,D A

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Pressure Gauge for Plasmas Subjected to Large Dynamic Electric and Magnetic Fields von Grabowsky, W. R., Durran, D. A., Gerard, M. E.

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