Ilim Lab

Ideal Heat Engine: Efficiency and the Carnot Limit

Compare heat-engine efficiency and test the Carnot limit across reservoir temperatures.

All Simulations

Apollo Parachute Descent

Configure Apollo’s parachute descent and see how deployment timing and Euler’s method affect a safe splashdown.

Apollo: Re-entry

Test Apollo return trajectories, hit the safe corridor, and see why mathematics and computation mattered for bringing the capsule home.