Engineers designing a scientific lander for an asteroid wish to include a simple…

PHYSICS · Multi-part · CBSE · Physics · Oscillations · Oscillations

Problem

Engineers designing a scientific lander for an asteroid wish to include a simple device for measuring the asteroid’s surface gravity. The lander carries a lightweight rigid rod and bob that can pivot freely to form a simple pendulum. After deployment, an onboard sensor measures the length of the pendulum to be 0.650 m±0.003 m0.650\,\text{m} \pm 0.003\,\text{m}. The lander then records the time required for 15 full oscillations as T15=23.4 s±0.1 sT_{15}=23.4\,\text{s} \pm 0.1\,\text{s} while the amplitude remains below 4∘4^{\circ}. (a) Derive an algebraic expression for the gravitational field strength gg on the asteroid in terms of the measured length ll and the average period TT. (b) Calculate the asteroid’s surface gravity using the measured values. Show all work, include units, and report your answer to an appropriate number of significant figures. (c) Determine the absolute uncertainty in the calculated value of gg by propagating the provided measurement uncertainties. (d) Suppose the asteroid has a radius of 350 m350\,\text{m} and is approximately spherical with uniform density. Using your value of gg, estimate the asteroid’s mass. State any additional assumptions clearly. (e) Comment on one limitation of using a simple pendulum for gravity measurements in the low-gravity environment of a small asteroid.

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