Add to ORKGCharts and graphs relative to magnetoplasmadynamic (MPD) thruster technology are given. The research activities at the Institute of Space Transportation, University of Stuttgart, are summarized. Information is given on the Institute's Electric Propulsion and Plasma Wind Tunnel; thermal arcjet research; the nozzle-type thruster, DT-IRS; nozzle-type MPD thrusters; a hot anode thruster; the DT6 thruster; the ZT-1 thruster; the cylindrical MPD thruster; and a comparison of continuous and quasi-steady MPD
Within the simulation limitations of on-orbit conditions, it was demonstrated that a helium purge sy...
Pressurizing gas heat transfer to liquid and wall in propellant tank for pressurant distributor desi...
THe original 12 cm hexagonal magneto-electrostatic containment discharge chamber has been optimized ...
The following topics are discussed: MMWe electric propulsion; MMWe thruster development; and coaxial...
On May 16, 1991, the NASA Headquarters Propulsion, Power, and Energy Division and the NASA Lewis Res...
Some of the topics covered with respect to the Lawrence Livermore National Laboratory's (LLNL's) con...
Inhouse magnetoplasmadynamic (MPD) thruster technology is discussed. The study focussed on steady st...
This document is presented in viewgraph form, and the topics covered include the following: (1) the ...
Performance data are presented for the tunnel, which has a Mach number range from 0.36 to 2.0. The t...
Radiation-cooled and water-cooled magnetoplasmadynamic thrustors tested in 10 to kW power range with...
The first detailed velocity profile data on thermally induced dust vortices are presented. These dus...
The focus of interest is the maneuvering flight of advanced entry vehicles operating at altitudes ab...
A ground test program was conducted to verify several of the design methods and techniques that were...
Major growth options for tended and manned space stations in LEO and GEO are examined including incr...
Heat transfer data for the 0.0175-scale space shuttle vehicle 3 are presented. Interference heating ...
Within the simulation limitations of on-orbit conditions, it was demonstrated that a helium purge sy...
Pressurizing gas heat transfer to liquid and wall in propellant tank for pressurant distributor desi...
THe original 12 cm hexagonal magneto-electrostatic containment discharge chamber has been optimized ...
The following topics are discussed: MMWe electric propulsion; MMWe thruster development; and coaxial...
On May 16, 1991, the NASA Headquarters Propulsion, Power, and Energy Division and the NASA Lewis Res...
Some of the topics covered with respect to the Lawrence Livermore National Laboratory's (LLNL's) con...
Inhouse magnetoplasmadynamic (MPD) thruster technology is discussed. The study focussed on steady st...
This document is presented in viewgraph form, and the topics covered include the following: (1) the ...
Performance data are presented for the tunnel, which has a Mach number range from 0.36 to 2.0. The t...
Radiation-cooled and water-cooled magnetoplasmadynamic thrustors tested in 10 to kW power range with...
The first detailed velocity profile data on thermally induced dust vortices are presented. These dus...
The focus of interest is the maneuvering flight of advanced entry vehicles operating at altitudes ab...
A ground test program was conducted to verify several of the design methods and techniques that were...
Major growth options for tended and manned space stations in LEO and GEO are examined including incr...
Heat transfer data for the 0.0175-scale space shuttle vehicle 3 are presented. Interference heating ...
Within the simulation limitations of on-orbit conditions, it was demonstrated that a helium purge sy...
Pressurizing gas heat transfer to liquid and wall in propellant tank for pressurant distributor desi...
THe original 12 cm hexagonal magneto-electrostatic containment discharge chamber has been optimized ...