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Thermal rocket
MULTIPHYSICS DESIGN and SIMULATION of a TUNGSTEN-CERMET NUCLEAR THERMAL ROCKET a Thesis by BRAD APPEL Submitted to the Office O
IAF Space Propulsion Symposium 2019
Energy Sources for Propulsion To, and for Distributed Use On, Mars
Feasibility and Performance of the Microwave Thermal Rocket Launcher
Space Exploration and Development Systems (SEEDS) 2014
(NTR) Artificial Gravity Mars Transfer Vehicle Concepts
Two-Stage-To-Orbit Transporting System Combining Microwave Rocket and Microwave Thermal Rocket for Small Satellite Launch
Movement and Maneuver in Deep Space: a Framework to Leverage Advanced Propulsion
Nuclear Thermal Rocket Simulation in NPSS
Nuclear Thermal Propulsion Systems (Last Updated in January 2021) Eric PROUST Eric Proust
Liquid Oxygen Augmented Gas Core Nuclear Thermal Rocket
Effects and Solutions on the Human Body After Long-Duration Space Flights
Human Lunar Mission Capabilities Using SSTO, ISRU and LOX-Augmented NTR Technologies- a Preliminary Assessment
FS&T Template
Internal Ballistics Simulation of a Solid Propellant Rocket Motor
Mission to Mars: How to Get People There and Back with Nuclear Energy
Nuclear Fission Power and Propulsion
NUCLEAR THERMAL ROCKET/VEHICLE CHARACTERISTICS and SENSITIVITY TRADES for NASA’S MARS DESIGN REFERENCE ARCHITECTURE (DRA) 5.0 STUDY
Top View
72Nd International Astronautical Congress 2021 the Interstellar Papers John I Davies
Stage-To-Orbit Nuclear Thermal Rocket
Operational Considerations for Fission Reactors Utilized on Nuclear Thermal Propulsion Missions to Mars
Tested and Analyzed Fuel Form Candidates for Nuclear Thermal Propulsion Applications
Los Alamos MASTER NATIONAL LABORATORY Los Alamos, New Mexico 8754S BF THIS DOCUMENT IS UNLIMITEB Contents
Design and Thermal Analysis of a Solar Thermal Thruster
In-Situ Alternative Propellants for Nuclear Thermal Propulsion Systems
4.2.1 Rockets and Launch Vehicles
Nuclear Pulse Propulsion
Nuclear Thermal Rocket
FINAL PROGRAM #Aiaapropenergy
Nuclear Space Propulsion: Overcoming the Chemical Barrier
Propulsion Cost Model Outline
Applying Newton's Laws
Nuclear Thermal Rocket Engine with a Toroidal Aerospike Nozzle
The Stratos Rocket Design, Simulation and Production of a Record Breaking Rocket
The Context and the Technological Challenges Propulsion System for Mars Exploration and Beyond
Assessment of the Advantages and Feasibility of a Nuclear Rocket for a Manned Mars Mission
69674 3 En Bookfrontmatter 1..61
Aerospace Propulsion Innovation Aerospace – Your Future November 03, 2012
Rstanding of Space, New Technology and Today’S Endeavors, Potential Missions in Space, and How Space Will Benefit All of Humanity
Proceedings of TVIW 2016 February 28-March 2, Chattanooga, TN
The Nuclear Cryogenic Propulsion Stage