The goal of the Nuclear Thermal Propulsion (NTP) technology development task is to determine the feasibility and affordability of using low enriched uranium (LEU) to power engines on a space transportation vehicle with solid cost and schedule confidence. This effort leverages government, industry and academic expertise to establish a conceptual design for a nuclear-powered rocket engine in the thrust range of interest for a human Mars mission.
More »Nuclear propulsion technology enables missions where solar-powered and chemical systems are limited. Faster transit propulsion for planetary missions combined with lowest total mission mass compared to chemical and solar electric. Improves crew safety. Nuclear propulsion technology provides a high-thrust, high-specific impulse capability that increases mission flexibility in cis-lunar space.
More »Organizations Performing Work | Role | Type | Location |
---|---|---|---|
Marshall Space Flight Center (MSFC) | Lead Organization | NASA Center | Huntsville, Alabama |
ACENT Laboratories LLC | Supporting Organization | Industry | Manorville, New York |
Florida Turbine Technologies, Inc. | Supporting Organization | Industry | Jupiter, Florida |
Glenn Research Center (GRC) | Supporting Organization | NASA Center | Cleveland, Ohio |
Idaho National Laboratory (INL) | Supporting Organization | FFRDC/UARC | Idaho Falls, Idaho |
Los Alamos National Laboratory (LANL) | Supporting Organization | FFRDC/UARC | Los Alamos, New Mexico |
Oak Ridge National Laboratory (ORNL) | Supporting Organization | FFRDC/UARC | Oak Ridge, Tennessee |
Quest Thermal Group | Supporting Organization | Industry | Arvada, Colorado |
Stennis Space Center (SSC) | Supporting Organization | NASA Center | Stennis Space Center, Mississippi |
Ultra Safe Nuclear Corporation-Technologies | Supporting Organization | Industry | Seattle, Washington |
Ultramet | Supporting Organization | Industry | Pacoima, California |