Final answer:
To calculate the fraction of a rocket's mass that must be destroyed to reach a low Earth orbit, we need to consider both the kinetic energy and gravitational potential energy needed.
Step-by-step explanation:
To calculate the fraction of a rocket's mass that must be destroyed to reach a low Earth orbit, we need to consider both the kinetic energy and gravitational potential energy needed.
The kinetic energy is given by the formula:
KE = (1/2)mv²
where m is the mass of the rocket and v is its velocity.
The gravitational potential energy is given by:
PE = mgh
where m is the mass of the rocket, g is the acceleration due to gravity, and h is the height of the orbit.
By using these formulas and the given orbital altitude of 250 km, we can calculate the fraction of the rocket's mass that must be destroyed.