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NEXT (ion thruster)
Magnetoshell Aerocapture: Advances Toward Concept Feasibility
Smallsat Aerocapture to Enable a New Paradigm of Planetary Missions
Study of a Crew Transfer Vehicle Using Aerocapture for Cycler Based Exploration of Mars by Larissa Balestrero Machado a Thesis S
Lifetime Assessment of the NEXT Ion Thruster
MPD Thruster Technology
Revolutionary Propulsion Research at Tu Dresden
Magnetoplasmadynamic Thruster with an Applied Field Based on the Second Generation High-Temperature Superconductors
Future Directions for Electric Propulsion Research
Movement and Maneuver in Deep Space: a Framework to Leverage Advanced Propulsion
Investigation of the Gem Mpd Thruster Using the Mach2 Magnetohydrodynamics Code
Liquid Oxygen Augmented Gas Core Nuclear Thermal Rocket
Current Status of NASA Evolutionary Xenon Thruster - Commercial (NEXT-C)
FS&T Template
Evaluation of the T5 (UK-10) Ion Thruster: Summary of Principal Results
Appendix I. NASA's Evolutionary Xenon Thruster (NEXT)
Nuclear Fission Power and Propulsion
Plasma, Ion-Thrusters, and VASIMR
HIGH-POWER SOLAR ELECTRIC PROPULSION in SPACE Joshua P
Top View
Neutron Star Systems 3 WHO WE ARE
NUCLEAR THERMAL ROCKET/VEHICLE CHARACTERISTICS and SENSITIVITY TRADES for NASA’S MARS DESIGN REFERENCE ARCHITECTURE (DRA) 5.0 STUDY
Modern In-Space Electric Propulsion
The Multimegawatt Program Taking Space Reactors to the Next Level
High Power MPD Thruster Development at the NASA Glenn Research Center
Advancements in the Demonstration of High Thrust to Power Ion Thruster
Nuclear Thermal Rocket/Vehicle Design Options for Future NASA Missions to the Moon and Mars
Status of Pulsed Inductive Thruster Research
Stage-To-Orbit Nuclear Thermal Rocket
Study of Feasibility of a Mission to Mars Using Aerocapture Technique
The 3D Fluid Simulations of the Solar Wind Interaction with Mars
4.2.1 Rockets and Launch Vehicles
Advances in Electric Propulsion
A Survey of Propulsion Options for Cargo and Piloted Missions to Mars∗
Solar Electric Propulsion (SEP) Systems for SMD Mission Needs
Electric Propulsion System – ION Thruster
Aerocapture Technology Developmnets by the In-Space
Performance Evaluation of the NEXT Ion Engine
KANUTER), for Future Space Applications
NASA's Evolutionary Xenon Thruster–Commerical (NEXT–C)
Hall Thrusters
Assessment of the Advantages and Feasibility of a Nuclear Rocket for a Manned Mars Mission
Oidtsaki Type: IQP Date: 5/2007 Project Number: JMW-NIAC
State-Of-The-Art and Advancement Paths for Inductive Pulsed Plasma Thrusters
Hall Effect Thruster Characterization Through Potential, Magnetic, and Optical Measurements Nicholas L
Aerojet Rocketdyne Receives Contract to Continue Development of NASA's Evolutionary Xenon Gridded Ion Thruster System