Space > 2. A Successful Rocket Launch >
Solve problems and analyse information using:
- Using Kepler’s third law.
- Right hand side remains constant for centre mass
- r = distance between mass centres of orbiting and central bodies, T = orbital period, M = mass of central body, G = gravitational constant (6.67 x 10-11 Nm2/kg)
- Re-arrange the equation as necessary