Research and experimental study for the development of a 1000 watt CW space environment S-band power amplifier
One thousand watt continuous wave space environment S band power amplifier development
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One thousand watt continuous wave space environment S band power amplifier development
Behavior of sloshing liquid column during acceleration reduction
Shock-panel coupling effects of supersonic turbulent flow driven by impedance head
Fluid mechanics information applied to gaseous nuclear rocket engines
Boundary layer development concerning turbulent flow with negligible heat transfer of Newtonian fluid in smooth annuli
Thin aluminum foil placed in magnetized plasma stream studied for lift drag ratio, noting magnetic field position influence on increase or decrease
Aerodynamic characteristics of minimum zero lift wave drag bodies at hypersonic speeds
Boundary layer development concerning turbulent flow with negligible heat transfer of Newtonian fluid in smooth annuli
Lip shock from separation edge of half angle wedge and resultant static pressure recovery distribution along wake
Nonequilibrium in 0.1-bar hydrogen arc using Balmer line and continuum emission coefficients and electron density from Stark broadened H beta line
Input admittances of imperfectly conducting dipole antennas in UHF range for various antenna lengths
High energy particle and electromagnetic space radiation effects on thermal control coating, noting spectral absorptance for various conditions
Pegasus thermal control louver system characteristics determined by environmental chamber testing, noting testing configuration
Near field characteristics of finite cylindrical antenna enclosed by long plasma sheath column, solving integral equations determining current distribution
Magnetofluid dynamic flow pressure distribution around sphere placed in aligned magnetic and velocity fields, noting drag and base pressure
Cathodic cleaning processes with plasma arc, preparing aluminum surfaces for arc welding
Particle clouds impingement effects, analyzing damages produced by exhaust from aluminized solid propellant rocket motors
No abstract available