How is the risk of a nuclear excursion or atmospheric release typically mitigated for an NTP system during the launch phase from Earth?
Answer
The system is designed to remain subcritical (non-operational) during launch and ascent, only becoming critical once safely in deep space.
The safety philosophy for launching fission reactors dictates that the reactor remains in a safe, non-operational state (subcritical) during the most hazardous part of the flight—launch and ascent—only activating once the spacecraft is far away from Earth.

Related Questions
What fundamentally separates Nuclear Thermal Propulsion (NTP) from conventional chemical rockets regarding energy application?What is the typical advantage in specific impulse ($I_{sp}$) that Nuclear Thermal Propulsion (NTP) systems offer over the most advanced chemical rockets?What is the primary operational benefit for crewed missions achieving a transit time reduction to Mars via NTP, such as cutting the trip to four or five months?How does Nuclear Electric Propulsion (NEP) differ from NTP in terms of thrust and application?Which radioactive isotope is most commonly utilized as the heat source in Radioisotope Thermoelectric Generators (RTGs)?What historical US programs successfully demonstrated the physics of nuclear thermal engines via ground testing?What is a major engineering hurdle for flight-ready NTP reactor systems beyond proving the core physics?How is the risk of a nuclear excursion or atmospheric release typically mitigated for an NTP system during the launch phase from Earth?What crucial balancing act must engineers perform when designing radiation shielding for crewed NTP missions?What strategic advantage does the high-thrust, high-$I_{sp}$ performance of NTP provide to mission planners concerning spacecraft design?What immediate next step is NASA taking to mature NTP technology, according to recent efforts mentioned?How does the safety discussion around launching RTGs differ fundamentally from launching NTP systems?