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Ion thruster
Propulsion Options for the Global Precipitation Measurement Core Satellite
Cave-73-02-Fullr.Pdf
Performance of the NASA 30 Cm Ion Thruster
Ionization Within a Plasma for the Purpose Investigating Space Propulsion and the Vasimr Plasma Rocket Engine
Degree at Master at Science Floyd J. Ruble, B.Sc
1 Iac-06-C4.4.7 the Innovative Dual-Stage 4-Grid Ion
Space Propulsion Technology for Small Spacecraft
Ion Propulsion
IGNITION! an Informal History of Liquid Rocket Propellants by John D
NASA's In-Space Propulsion Technology Program: Overview And
Development of the Radio Frequency Ion Thruster RIT XT
Xenon Ion Propulsion for Orbit Transfer
Future Directions for Electric Propulsion Research
Analysis of a Miniature Radio Frequency Ion Thruster with an Induc- Tively Coupled Plasma Source
Development Status of High-Thrust Density Electrostatic Engines
Rocket and Spacecraft Propulsion Principles, Practice and New Developments (Third Edition)
Plasma Propulsion for Rocket Engine Using Ion Thruster
Radio-Frequency Ion Thrusters Power Measurement and Power
Top View
In-Space Propulsion Program Overview and Status
Nuclear Electric Propulsion: Assessing the Design of Project Prometheus
Electric Propulsion and Electric Satellites
Performance Characterization of a Helicon Double Layer Thruster Using Direct Thrust Measurements Sabrina Pottinger, Vaios Lappas, Christine Charles, Rod Boswell
XIPS Ion Thrusters for Small Satellite Applications
An Overview of Cube-Satellite Propulsion Technologies and Trends
Plasma, Ion-Thrusters, and VASIMR
Modern In-Space Electric Propulsion
Electric Propulsion and Plasma Dynamics Laboratory
1 ANALYSIS of HALL-EFFECT THRUSTERS and ION ENGINES for ORBIT TRANSFER MISSIONS Frank S. Gulczinski III*, Ronald A. Spores**
A Fluidic Alternative to the EM Drive Propulsion Concept: the Orthogonal Fluid Flow Propulsion Concept
Overview of US Academic Programs in Electric Propulsion
Overview of Sail Propulsion for Space Flight
The 3D Fluid Simulations of the Solar Wind Interaction with Mars
Ion Beam Shepherd Report
Study of Helicon Double Layer Thruster
Investigation of a Space Propulsion Concept Using Inertial Electrostatic Confinement
Permanent Magnet Helicon Source for Ion Propulsion Francis F