Final answer:
The pressure inside the hot aerosol can will be approximately 67.29 atm.
Step-by-step explanation:
To determine the pressure inside the hot aerosol can, we can use the ideal gas law equation: PV = nRT, where P is the initial pressure, V is the initial volume, n is the number of moles, R is the ideal gas constant, and T is the temperature.
First, convert the initial pressure of 1.20 atm to torr by multiplying by 760: 1.20 atm * 760 torr/atm = 912 torr. Next, convert the initial temperature of 22 °C to Kelvin by adding 273: 22 °C + 273 = 295 K.
Now, we can use the ideal gas law to find the pressure inside the hot can. Rearranging the equation to solve for P, we have P = (nRT)/V. Since the can is empty except for the propellant gas, the moles of gas remain the same. Plug in the known values:
P = (n * R * T_hot) / V
P = (n * R * 545 + 273) / V = (n * R * 818) / V
Finally, substitute the values: P = (n * R * 818) / V = (1 * 0.0821 * 818) / 1 = 67.2858 atm
The pressure inside the hot can will be approximately 67.29 atm.