Answer all the questions in the spaces provided. (b) A rocket is launched from the surface of a planet and moves along a radial path, as shown in Fig. 1.1. planet mass M A R R 4R Fig. 1.1 B rocket path The planet may be considered to be an isolated sphere of radius R with all of its mass M concentrated at its centre. Point A is a distance R from the surface of the planet. Point B is a distance 4R from the surface.
- (a)Define gravitational potential at a point.[2]
- (b)(i)Show that the difference in gravitational potential Δφ between points A and B is given by the expression Δφ = 3GM / 10R where G is the gravitational constant.[1]
- (b)(ii)The rocket motor is switched off at point A. During the journey from A to B, the rocket has a constant mass of 4.7 × 10⁴ kg and its kinetic energy changes from 1.70 TJ to 0.88 TJ. For the planet, the product GM is 4.0 × 10¹⁴ Nm² kg⁻¹. It may be assumed that resistive forces to the motion of the rocket are negligible. Use the expression in (b)(i) to determine the distance from A to B.[3]
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Mark scheme
Marking points from the official mark scheme (Feb/Mar 2017). The mark or mark type is shown in brackets.
- [M1] work done per unit mass
- [A1] bringing (small test) mass from infinity (to the point)
- [A1] ∆φ = (GM/2R) – (GM/5R) = 3GM/10R
- [C1] change in GPE = (3 × 4.0 × 10¹⁴ / 10 R) × 4.7 × 10⁴
- [C1] (3 × 4.0 × 10¹⁴ / 10 R) × 4.7 × 10⁴ = (1.70 – 0.88) × 10¹²
- [A1] R = 6.88 x10⁶ (distance = 3 × 6.88 ×10⁶ = 2.1 x 10⁷ m)
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