Conceptual Engine System Design for NERVA derived 66.7KN and 111.2KN Thrust Nuclear Thermal Rockets
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AIP
Cited by 6 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. The Bimodal Epithermal Astronuclear Reactor (BEAR): A LONG-LIVED, Universal Space Nuclear Powerplant;Nuclear Science and Technology Open Research;2024-02-01
2. Numerical Simulation of Thermal-Hydrodynamic Transients in the Cooling Channels of a Nuclear Thermal Propulsion Engine;50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference;2014-07-25
3. Parametric Analyses of a 75 kN Thrust Class Composite Fuel Based NTR Engine;50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference;2014-07-25
4. Integrated Propulsion and Power Modeling for Bimodal Nuclear Thermal Rockets;43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2007-07-08
5. Multidisciplinary Analysis of Nuclear Thermal Propulsion Design Options for Human Exploration Missions;42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2006-07-09
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