Final answer:
The minimum initial speed of the projectile to reach a height of 2.55 × 10^6 m above the satellite's surface can be calculated using the concept of gravitational potential energy.
Step-by-step explanation:
To calculate the minimum initial speed of the projectile to reach a height of 2.55 × 10^6 m above the satellite's surface, we can use the concept of gravitational potential energy. The gravitational potential energy at the surface of the satellite can be calculated using the formula:
PE = -GMm/r, where G is the gravitational constant, M is the mass of the satellite, m is the mass of the projectile, and r is the radius of the satellite.
At the highest point of the projectile's trajectory, all of its initial kinetic energy will have been converted to potential energy. So, we can equate the initial kinetic energy to the change in potential energy:
KE = PE
1/2 mv^2 = -GMm/r + GMm/(r + h), where v is the initial speed of the projectile and h is the vertical height above the surface.
By substituting the given values, we can solve for v:
v = sqrt((2GM/r) + (2GM/(r + h))).