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Nuclear Thermal Propulsion Development RisksThere are clear advantages of development of a Nuclear Thermal Propulsion (NTP) for a crewed mission to Mars. NTP for in-space propulsion enables more ambitious space missions by providing high thrust at high specific impulse ((is) approximately 900 sec) that is 2 times the best theoretical performance possible for chemical rockets. Missions can be optimized for maximum payload capability to take more payload with reduced total mass to orbit; saving cost on reduction of the number of launch vehicles needed. Or missions can be optimized to minimize trip time significantly to reduce the deep space radiation exposure to the crew. NTR propulsion technology is a game changer for space exploration to Mars and beyond. However, 'NUCLEAR' is a word that is feared and vilified by some groups and the hostility towards development of any nuclear systems can meet great opposition by the public as well as from national leaders and people in authority. The public often associates the 'nuclear' word with weapons of mass destruction. The development NTP is at risk due to unwarranted public fears and clear honest communication of nuclear safety will be critical to the success of the development of the NTP technology. Reducing cost to NTP development is critical to its acceptance and funding. In the past, highly inflated cost estimates of a full-scale development nuclear engine due to Category I nuclear security requirements and costly regulatory requirements have put the NTP technology as a low priority. Innovative approaches utilizing low enriched uranium (LEU). Even though NTP can be a small source of radiation to the crew, NTP can facilitate significant reduction of crew exposure to solar and cosmic radiation by reducing trip times by 3-4 months. Current Human Mars Mission (HMM) trajectories with conventional propulsion systems and fuel-efficient transfer orbits exceed astronaut radiation exposure limits. Utilizing extra propellant from one additional SLS launch and available energy in the NTP fuel, HMM radiation exposure can be reduced significantly.
Document ID
20150006889
Acquisition Source
Marshall Space Flight Center
Document Type
Abstract
Authors
Kim, Tony
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
April 29, 2015
Publication Date
February 23, 2015
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
M15-4269
Report Number: M15-4269
Meeting Information
Meeting: Nuclear and Emerging Technologies for Space 2015 (NETS)
Location: Albuquerque, NM
Country: United States
Start Date: February 23, 2015
End Date: February 26, 2015
Sponsors: American Nuclear Society, National Nuclear Laboratory-Central Laboratory, Aerojet Rocketdyne, Inc.
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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