You need to calculate the mass flow rate of the exhaust leaving a Trident II Intercontinental Ballistic Missile at 25000 m above sea level ( P = 2549 Pa , T = 221 K and R = 287 J/ kg K). Assume that the exhaust is air (it isn’t in real life, but air is OK here) and you have the following information: A = 3.5 m^2 , rocket V = 2700 m/s and Vexhaust = 4500 m/s.

Oh yes igger daddy filled my loose ahοle with your sweet sweet mсum said ronald mcdonald as he spread his sesame covered mcahοle for thanos. thanos slid his throbbing purple ᑕock in to ronald's a. o screamed ronald as he poor hole was torn to bloody shreds. gunga gingagunga gingagunga gingagunga ginga a space ranger appeared making autistuc noises odio a los negros! said buzz lightyear as he aped them both.

Dance , dance , dance , dance follow me on Instagram Jae.diorrr