Equilibrium Emissivity Calculations for a Hydrogen Plasma at Temperatures Up to 10,000 0 K
DESIGN, FABRICATION, AND TESTING OF A CESIUM ION ROCKET ENGINE.
DESIGN, FABRICATION, AND TESTING OF A CESIUM ION ROCKET ENGINE.
Re-Entry Physics. Volume III. Interaction of Vehicles in Early Re-Entry Environment. Chapters 1-5
Representation of Propagation Parameters for the Plasma in a Magnetic Field
RESEARCH & DEVELOPMENT STUDY OF A MAGNETIC INDUCTION PLASMA ENGINE.
DESIGN, FABRICATION, AND TESTING OF A CESIUM ION ROCKET ENGINE - PHASE II.
RESEARCH AND DEVELOPMENT OF A 1 KW PLASMAJET THRUSTER
ASTRONAUTICS INFORMATION. ELECTRICALLY PROPELLED SPACECRAFT AND ASSOCIATED SUBJECTS
THE EFFECT OF VELOCITY DISTRIBUTIONS ON POWER-LIMITED PROPULSION SYSTEM
The use of a coaxial gun for plasma propulsion Final report