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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
Bibliography No. 39-3
Electric Propulsion
United States Patent 19 11) 4,091,769 Baldwin (45) May 30, 1978
SP2018 Technical Program
Design and Performance Analysis Study of an Ion Thruster
RIT-Μx - the New Modular High Precision Micro Ion Propulsion System
Feasibility Study of Low Power Helicon Thruster M
4.2.1 Rockets and Launch Vehicles
NASA In-Space Propulsion Systems Technology Area Roadmap
An RF Plasma Thruster for Use in Small Satellites Dr
Programme Content
FINAL PROGRAM #Aiaapropenergy
Nuclear Space Propulsion: Overcoming the Chemical Barrier
Advances in Electric Propulsion
Time-Optimal Trajectories to Circumsolar Space Using Solar
Micro RF Ion Engine for Small Satellite Applications
Electric Propulsion System – ION Thruster
NASA's In-Space Propulsion Technology Program
Ion Thruster Thrust Vectoring Requirements and Techniques
A Review of Electrodynamic Tethers for Space Applications
Electric Propulsion Methods for Small Satellites: a Review
Comparison of Four Space Propulsion Methods for Reducing Transfer Times of Crewed Mars Mission
Physics and Applications of Electrodynamic Space Tethers
Creation and Analysis of an Electric and Magnetic Model of a Micro Ion Thruster
Design of an Air-Breathing Electric Thruster for Cubesat Applications
Demaio Umd 0117N 11210.Pdf
Plasma and Nuclear Propulsion
Full Text [PDF]
Development and Testing of Electric and Advanced Propulsion Systems
Updated Performance Measurements and Analysis of the Phase Four RF Thruster
Investigation of a Cluster of High Power Helicon Thrusters For
8. Electric Propulsion of Spacecraft and Rockets
An Orbital Dynamics Model for an Ultra-Low Altitude Lunar Orbiter