During the powered ascent of a small test rocket

PHYSICS · Multi-part · A Level · Physics · Mechanics and materials · Mechanics and materials

Problem

During the powered ascent of a small test rocket, onboard instrumentation records that the engine’s power output increases linearly with time, from P0=1.0×102 WP_0 = 1.0\times10^{2}\,\text{W} at launch (t=0t=0) to Pf=7.0×102 WP_f = 7.0\times10^{2}\,\text{W} at t=4.0 st=4.0\,\text{s}. Throughout this interval the rocket’s mass remains effectively constant, and all engine power is converted into the rocket’s mechanical energy. (a) Derive an algebraic expression for the power P(t)P(t) as a function of time tt during the 4-s burn. (b) Determine the exact amount of work performed by the engine on the rocket during the burn, expressing your answer in joules. (c) Calculate the rocket’s average power output over the 4-s interval and verify that it matches an appropriate geometric interpretation of the power–time graph. (d) Discuss what the positive slope of P(t)P(t) implies about the engine’s operating conditions or fuel-combustion characteristics during the burn.

Related theory

Browse the problem library