Write a function called empirical_sample_mean_sd that takes a sample size n as its argument. the function should simulate 500 samples with replacemnt of size n from the flight delays dataset, and it should return the standard deviation of the means of those 500 samples. hint: this function will be similar to the sample_size_n function you wrote earlier.

Aspacecraft can attain a stable orbit 300 kilometers above earth if it reaches a velocity of 7.7 kilometers per second. the formula for a rocket's maximum velocity v in kilometers per second is vequalsminus0.0098tplusc ln upper r, where t is the firing time in seconds, c is the velocity of the exhaust in kilometers per second, and r is the ratio of the mass of the rocket filled with fuel to the mass of the rocket without fuel. find the velocity of a spacecraft whose booster rocket has a mass ratio of 20, an exhaust velocity of 2.1 km/s, and a firing time of 15 s. can the spacecraft achieve a stable orbit 300 km above earth?