Assertion: turbine's thrust | /r/CapableOf | increase net thrust
Facets:
value: at the nozzle exit plane
type: LOCATION
Source sentences:
text: At any given throttle, the thrust and efficiency of a rocket motor improves slightly with increasing altitude (because the back-pressure falls thus increasing net thrust at the nozzle exit plane), whereas with a turbojet (or turbofan) the falling density of the air entering the intake (and the hot gases leaving the nozzle) causes the net thrust to decrease with increasing altitude.