Calculate the force of gravity on a spacecraft

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Homework Help Overview

The problem involves calculating the force of gravity on a spacecraft located 19200 km above the Earth's surface, with a specified mass of 1500 kg. The context is centered around gravitational force equations and the implications of distance measurements in physics.

Discussion Character

  • Exploratory, Assumption checking

Approaches and Questions Raised

  • Participants discuss the correct interpretation of the distance variable in the gravitational force equation, questioning whether it should be measured from the Earth's surface or the center of the Earth. There are attempts to recalculate the gravitational force based on different interpretations of the radius.

Discussion Status

The discussion is ongoing, with participants exploring different interpretations of the problem setup. Some guidance has been offered regarding the importance of accurately understanding the distance measurement in gravitational calculations.

Contextual Notes

There is a noted emphasis on the potential for confusion in interpreting altitude versus radius in gravitational equations, highlighting common pitfalls in physics problems.

mathcrzy
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1. Homework Statement

Calculate the force of gravity on a spacecraft 19200 km (3 Earth radii) above the Earth's surface if its mass is 1500 kg.


2. Homework Equations

Fg=[(G)(M spacecraft )(Mearth)]/r^2=ma.

3. The Attempt at a Solution

a=[(6.67e-11)(1500)(6e24)]/19200000^2(convert km to m)=1628.4
 
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mathcrzy said:
1. Homework Statement

Calculate the force of gravity on a spacecraft 19200 km (3 Earth radii) above the Earth's surface if its mass is 1500 kg.


2. Homework Equations

Fg=[(G)(M spacecraft )(Mearth)]/r^2=ma.

3. The Attempt at a Solution

a=[(6.67e-11)(1500)(6e24)]/19200000^2(convert km to m)=1628.4

Whoops! Ya fell into the pit -- they catch lots of students this way (especially on multiple choice questions). What does r represent in Newton's gravitational force equation? The distance you are given is measured from the surface of the Earth, that is, it is an altitude... (Oh, and don't forget to put units on your answers!)
 
r represents the radius and so it would be 4 Earth radii because they only talk about from the surface? so if that is the case i would do a=[(6.67e-11)(1500)(6e24)]/25600000^2(convert km to m)=915.98N
 
mathcrzy said:
r represents the radius and so it would be 4 Earth radii because they only talk about from the surface? so if that is the case i would do a=[(6.67e-11)(1500)(6e24)]/25600000^2(convert km to m)=915.98N

That looks fine! Be sure to read exam problems carefully because little traps like this are frequently set for the unwary. (Altitude is more convenient for describing orbits, and people who work with Earth satellites do so all the time, but the value always has to be adjusted to distance from the center of Earth for use in equations.)
 

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