Concept illustration of the engine

All directions

SPRINT · 01

D–T energy balance

Neutrons carry most of the reaction energy. Recovering it as thrust is the central problem of this workstream.

Established physics

Neutrons carry most of the D–T fusion energy.

Deuterium–tritium fusion produces a helium nucleus (an alpha particle) and a neutron. About one fifth of the energy goes to the alpha particle and the rest to the neutron. This is textbook physics, not an assumption.

A magnetic nozzle can only steer charged particles. The neutron has no charge and passes straight through the field. So if only charged products feed the exhaust, the engine uses just a small part of the fusion energy.

The model question

Recovering neutron energy in the propellant.

In the SPRINT concept the target is surrounded by propellant in the form of a plasma liner. Some neutrons are absorbed there and heat it, and that heated, charged material leaves through the nozzle. The model has to show what share of the neutron energy the liner can actually capture and pass on to the exhaust.

exhaust power = nozzle efficiency × (alpha-particle energy + share of neutron energy captured by the propellant)

Whatever does not reach the exhaust does not vanish: neutrons that miss the liner heat the shield and coils, and radiation goes to the radiators. The model must account for every one of these terms.

What we test

Parameters that determine the energy balance.

ParameterStatusWhat we test
Alpha-particle energy shareknownA tabulated value for D–T; not adjustable
Fusion yield per pulseunder studyWhether it is realistic at the given compression; NIF results are the benchmark
Pulse rateunder studyWhether target delivery and system recharge can keep up
Neutron capture by the propellantkey questionHow much neutron energy the liner absorbs and how much goes to the shield
Magnetic nozzle efficiencyunder studyWhat share of plasma energy becomes directed flow