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Glossary / Nuclear Thermal Propulsion (NTP)
Propulsion

Nuclear Thermal Propulsion (NTP)

A propulsion concept that uses a nuclear reactor to heat propellant, offering roughly twice the specific impulse of chemical rockets for deep-space missions.

Nuclear Thermal Propulsion (NTP) works by passing a propellant, usually liquid hydrogen, through a nuclear fission reactor core, heating it to extreme temperatures before expelling it through a nozzle. NTP can theoretically achieve specific impulse of 850-1,000 seconds, roughly double that of the best chemical engines, while providing thrust levels high enough for crewed deep-space missions.

NASA and DARPA are jointly developing the DRACO (Demonstration Rocket for Agile Cislunar Operations) program to flight-test an NTP engine by the late 2020s. NTP is widely considered the most promising technology for reducing Mars transit times from 7-9 months to approximately 3-4 months, significantly reducing crew radiation exposure and mission risk.

Related Terms

Cislunar Space
Delta-v
Specific Impulse (Isp)
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