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The Analysis of Turbine Propulsion Systems in Nuclear Submarines
Mars Mission Analysis Trades Based on Legacy and Future Nuclear Propulsion Options
Application of Solar-Electric Propulsion to Robotic Missions in Near-Earth Space
Paris to Hektor: A Concept for a Mission to the Jovian Trojan Asteroids
Titan Exploration Using a Radioisotopically-Heated Montgolfier Balloon
Summary of NR Program Prometheus Efforts
High Performance Lightweight Compact Thermal Radiator for Space Vehicles
A New Capability for Nuclear Thermal Rocket Propulsion Design
Ex-Core CFD Analysis Results for the Prometheus Gas Reactor
Key Factors Influencing the Decision on the Number of Brayton Units for the Prometheus Space Reactor
Status Update of a Free-Piston Stirling Convertor for Radioisotope Space Power Systems
Development and Characterization of Solid Solution Tri-Carbides
Magnetized Target Fusion for Advanced Space Propulsion
Mass Estimates of Very Small Reactor Cores Fueled by Uranium-235, U-233 and Cm-245
Coupled Reactor Kinetics and Heat Transfer Model for Heat Pipe Cooled Reactors
Chemical Analysis of Plutonium-238 for Space Applications
Application of Nuclear Photon Engines for Deep-Space Exploration
High Density Storage of Antimatter for Space Propulsion Applications
Multimegawatt Nuclear Electric Propulsion with Gaseous and Vapor Core Reactors with MHD
Development of Core Cladding Fabrication Techniques for Phase I Fission Propulsion Systems
Options for Development of Space Fission Propulsion Systems
A High Power, Coated Particle Fuel Compact Radioisotope Heat Unit
Milliwatt Radioisotope Power Supply for the PASCAL Mars Surface Stations
Interstellar Travel-Challenging Propulsion and Power Technologies for the Next 50 Years
A Novel Thin Film Dispenser Cathode for Thermionic Emission
Application of Revised Thermionic Theory to MTC Diodes
Metallurgical Examination of an AMTEC Unit
Oxidation of Mo-Re at Reduced Oxygen Pressures
Modular Stirling Radioisotope Power System (SRPS) Using an Advanced Heat Source
Advanced Research Interplanetary Exploration Ship (A.R.I.E.S.)
A Possible Propellantless Propulsion System
Thermal Vacuum Testing of a MHW RTG AFter 17 Years in Storage
Radioisotope Power System Options for Future Planetary Missions
Mathematical Modeling of the Impedance of Single and Multi-cell AMTEC Units
Advanced Radioisotope Heat Source for Stirling Engines
Results of 30 kWt Safe Affordable Fission Engine (SAFE-30) Primary Heat Transport Testing
High Efficiency Segmented Thermoelectric Unicouples
High Efficiency Segmented Thermoelectric Unicouples
Concept for High Performance MHD Airbreathing-IEC Fusion Rocket
Design and Preliminary Testing of a High Performance Antiproton Trap (HiPAT)