Parameter

4.6.3.6 nuclear based propulsion

A propulsion system that uses nuclear energy to generate power, such as nuclear reactors (fission-based), nuclear thermal propulsion (NTP), or radioisotope thermoelectric generators (RTGs), to propel an aircraft or spacecraft. This technology offers a potential source of long-duration, high-energy density power, enabling missions that would be impossible with conventional propulsion. While not currently used for commercial aircraft (due to weight, safety, and regulatory concerns), nuclear propulsion is used for spacecraft like Voyager, Cassini, and Mars rovers, providing zero-emission, high-energy-density power for deep space exploration.

Hierarchy

4 technological themes
4.1 active aircraft control
4.2 data transfer technologies
4.3 energy carriers
4.4 net zero technologies
4.5 operational technologies
4.6 aircraft propulsion
4.6.1 propulsor integration on airframe
4.6.2 converting shaft power to thrust
4.6.3 converting fuel to shaft power
4.6.3.1 gas turbine water injection from h2 fuel cells
4.6.3.2 exhaust heat energy recovery
4.6.3.3 new combustion for premixed (clean) fuels
4.6.3.4 waste heat recovery for lh2 to gh2 (preconditioning)
4.6.3.5 hydrogen fuel cells
4.6.3.6 nuclear based propulsion
4.6.4 non-combustion based engine integration
4.6.5 other propulsion technologies
4.7 aircraft structures

Scenario relevance

Number of parameter occurrence per scenario.

Input
Output
1
1
Optimising together
N/A
Stripping down
N/A
Tech for you
N/A
Mad max

Milestone Timehorizon

PESTEL categories

Current

Short term

Medium term

Long term

Little to many relations with other Milestones