In order to calculate the speed of the spacecraft, use the following formula;
![v=\sqrt[]{(GM)/(r)}](https://img.qammunity.org/2023/formulas/physics/college/r7hw78zus5n8dwgxbm7kieugeby64cwf2j.png)
where,
M: mass of the moon = 7.3*10^22 kg
G: Cavendish constant = 6.67*10^-11 Nm^2/kg^2
r: distance in between the spacecraft and the center of the Moon =
172 km + 1840 km = 2012 km
Replace the previous values of the parameters into the formula for v and simplify:
![v=\sqrt[]{\frac{(6.67\cdot10^(-11)N\frac{m^2}{\operatorname{kg}^2})(7.3\cdot10^(22)kg)}{2012\operatorname{km}}}\approx4.91\cdot10^4(m)/(s)]()
Hence, the speed of the spacecraft is approximately 4.91*10^4 m/s