Concept

Rocket equation — where it appears

The relation between a rocket's gain in speed and the fraction of its mass burned: the speed gained is the exhaust speed times the logarithm of the mass ratio. It follows from momentum conservation alone, and its logarithm is why high speeds demand so much propellant.

Named by 2 essays across 2 fields — each of them below, with the objects they name alongside it.

Named alongside it

The objects these essays reach for when they reach for this one.

AblationAreal densityBurn fractionCentral hot spotExhaust velocityFermi pressureHohlraumInertial confinementInterstellar travelE = mc²Mass ratioMomentum

All concepts