Assertion: engine's thrust | /r/HasProperty | vac
Facets:
Source sentences:
text: Where F N {\displaystyle F_{N}} is the net thrust, I sp,vac {\displaystyle I_{\text{sp,vac}}} is the specific impulse, g 0 {\displaystyle g_{0}} is a standard gravity, m ˙ {\displaystyle {\dot {m}}} is the propellant flow in kg/s, A e {\displaystyle A_{e}} is the cross-sectional area at the exit of the exhaust nozzle, and p {\displaystyle p} is the atmospheric pressure.