论文信息 - NTP Design Derivatives and Enhancements for Lunar and Mars Missions - 字舞流文

NTP Design Derivatives and Enhancements for Lunar and Mars Missions

Claude R. Joyner | Daniel J. Levack | Christopher B. Reynolds | Timothy S. Kokan | David Hanks | Michael Eades | Tyler Jennings | C. Joyner | Christopher Reynolds | M. Eades | T. Kokan | D. Hanks | Tyler Jennings | D. Levack

[1] Stanley K. Borowski,et al. "2001: A Space Odyssey" Revisited—The Feasibility of 24 Hour Commuter Flights to the Moon Using NTR Propulsion with LUNOX Afterburners , 1997 .

[2] Paolo Venneri,et al. A feasibility study on low-enriched uranium fuel for nuclear thermal rockets – I: Reactivity potential , 2015 .

[3] John Crowley,et al. Determining Mars Mission NTP Thrust Size and Architecture Impact for Mission Options , 2015 .

[4] Claude R. Joyner,et al. Comparing Low Enriched Fuel to Highly Enriched Fuel for use in Nuclear Thermal Propulsion Systems , 2016 .

[5] James F. Horton,et al. Enabling Multiple Abort Strategies Using the NTP Approach for Human Mars Missions , 2017 .

[6] C. Joyner,et al. NTP Design Sensitivities for Human Lunar and Mars Missions , 2018, 2018 Joint Propulsion Conference.