3-D plasma armature railgun simulations
4th Symposium on Electromagnetic Launch Technology, 12-14 April 1988, Austin, TX, USA
About the Calculation of a Discharge Coil with Given Distribution of the Induced Electric Field
Active control of a high Reynolds number Mach 0.9 axisymmetric jet
Active control of a Mach 0.9 jet for noise mitigation using plasma actuators
Advanced carbon-based material as space radiation shields
Advanced sintering of garnet-based ceramic composite cathodes for all-solid-state lithium batteries
A fault tolerant control computer for the Aspera plasma instrument of Phobos spacecraft
Analyses of molecular and neutral atomic emission spectra from an electrothermal launcher plasma
Analyse von heißen Hyperschallströmungen um Steuerklappen mit Fluid-Struktur-Wechselwirkung
Analysis of plasma loss in a ring-cusp ion thruster
An approximation method to calculate the radiation of strong shock waves in argon
Application of artificial neural networks for spacecraft instrument data compression
Application of the plasma-MIG technology for the joining of galvanised steel materials
Applied Thermionic Research Quarterly Progress Report, 25 Jan. - 25 Mar. 1965