Some of the topics covered with respect to the Lawrence Livermore National Laboratory's (LLNL's) contributions to Magnetoplasmadynamic (MPD) Thrusters for the Space Exploration Initiative (SEI) include: an IR camera, plasma-induced erosion/redeposition, the Mirror Fusion Test Facility-B (MFTF-B), the Thruster Lifetime Test Facility, the RACE Compact Torus Accelerator Facility, and a RACE program summary. Some of the other topics addressed include: flux contours for HAM simulation, comparison of RACE data of plasma ring formation with the HAM 2-D magnetohydrodynamic code, and the 2-D Ring Acceleration Code (TRAC)
A ground test program was conducted to verify several of the design methods and techniques that were...
Magnetoplasmadynamics (MPD) arc devices have been operated at power levels from 10 KW to 0.1 MW. Whe...
Experimental data were combined with one-dimensional conservation relations to yield information on ...
The following topics are discussed: MMWe electric propulsion; MMWe thruster development; and coaxial...
Charts and graphs relative to magnetoplasmadynamic (MPD) thruster technology are given. The research...
Research was initiated in advanced plasma thrusters that capitalizes on lab capabilities in plasma s...
The topics are presented in viewgraph form and include the following: overall strategy for magnetopl...
Inhouse magnetoplasmadynamic (MPD) thruster technology is discussed. The study focussed on steady st...
Current density determines the plasma flow regime. Cascades are non-stationary. ALWAYS. All flow reg...
The following topics are discussed: a whistler-based electron cyclotron resonance heating (ECRH) thr...
Laboratory tests with simulated micrometeoroids to measure the heat transfer coefficient are discuss...
On May 16, 1991, the NASA Headquarters Propulsion, Power, and Energy Division and the NASA Lewis Res...
The topics covered are presented in viewgraph form and include the following: engine lifetime assess...
The development of lithium magnetoplasmadynamic (MPD) thrusters at JPL is discussed. The following t...
Heat transfer data for the 0.0175-scale space shuttle vehicle 3 are presented. Interference heating ...
A ground test program was conducted to verify several of the design methods and techniques that were...
Magnetoplasmadynamics (MPD) arc devices have been operated at power levels from 10 KW to 0.1 MW. Whe...
Experimental data were combined with one-dimensional conservation relations to yield information on ...
The following topics are discussed: MMWe electric propulsion; MMWe thruster development; and coaxial...
Charts and graphs relative to magnetoplasmadynamic (MPD) thruster technology are given. The research...
Research was initiated in advanced plasma thrusters that capitalizes on lab capabilities in plasma s...
The topics are presented in viewgraph form and include the following: overall strategy for magnetopl...
Inhouse magnetoplasmadynamic (MPD) thruster technology is discussed. The study focussed on steady st...
Current density determines the plasma flow regime. Cascades are non-stationary. ALWAYS. All flow reg...
The following topics are discussed: a whistler-based electron cyclotron resonance heating (ECRH) thr...
Laboratory tests with simulated micrometeoroids to measure the heat transfer coefficient are discuss...
On May 16, 1991, the NASA Headquarters Propulsion, Power, and Energy Division and the NASA Lewis Res...
The topics covered are presented in viewgraph form and include the following: engine lifetime assess...
The development of lithium magnetoplasmadynamic (MPD) thrusters at JPL is discussed. The following t...
Heat transfer data for the 0.0175-scale space shuttle vehicle 3 are presented. Interference heating ...
A ground test program was conducted to verify several of the design methods and techniques that were...
Magnetoplasmadynamics (MPD) arc devices have been operated at power levels from 10 KW to 0.1 MW. Whe...
Experimental data were combined with one-dimensional conservation relations to yield information on ...