Why Are Units and Significant Figures Crucial in Scientific Calculations?

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SUMMARY

The discussion focuses on the importance of units and significant figures in scientific calculations, specifically in the context of calculating angular velocity and period for a satellite orbiting Earth. The student's calculated angular velocity of 0.0002 rad/s is deemed unacceptable due to improper application of significant figures, leading to an erroneous period of 31415.92 seconds. The correct interpretation of results requires adherence to significant figures to ensure precision and accuracy. The discussion emphasizes that scientific notation should be utilized to express values appropriately, particularly in cases involving small quantities.

PREREQUISITES
  • Understanding of angular velocity and its units
  • Knowledge of significant figures and their application in calculations
  • Familiarity with gravitational force equations
  • Basic principles of satellite motion and centripetal force
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  • Study the application of significant figures in scientific calculations
  • Learn about angular velocity calculations in orbital mechanics
  • Explore gravitational force equations and their implications in satellite motion
  • Review scientific notation and its importance in expressing small values
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Students in physics, educators teaching scientific principles, and anyone involved in precise scientific calculations will benefit from this discussion.

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Homework Statement



A student recently submitted a homework solution in which he or she had calculated
an angular velocity w = 0.0002 rad/s (for a satellite going around the Earth.) The
student then found the period by using T = rad /w = 31415.92 seconds. Describe why
both answers are unacceptable. This is not about any formulae — it is about the
results that are given. (Your discussion should contain 4 or 5 sentences at the least.)

Homework Equations



N/A

The Attempt at a Solution



I think scentific notation should be applied, but other than that? Not sure what they want.

TIA
 
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When a satellite going around the Earth, the centripetal force is provided by the gravitational froce of Earth on the satellite.
Hence m*w^2*R = GMm/R^2. Where R is the radius of the Earth and M is the mass of the earth. Where close to the Earth GM = gR^2 where g s the acceleration due to gravity. Using these values calculate w. and verify the result with the given value.
 

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