NEXT (ion thruster)
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