Initial speed of an object launched from Mars

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SUMMARY

The discussion centers on calculating the initial speed of an object launched from Mars using gravitational potential energy and kinetic energy equations. The user initially miscalculated the speed due to incorrect unit conversion of the radius (r) from kilometers to meters. After correcting the unit, the final calculated initial speed (vi) is approximately 153,776.815 m/s, derived from the formula vi = √(vf^2 + (2GMm)/r) with G as 6.7 E-11 and Mars' mass as 6 E23 kg.

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marjine
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Homework Statement
The radius of Mars (from the center of just above the atmosphere) is 3400 km, and its mass is 6 × 1023 kg. An object is launched straight up from just above the atmosphere of Mars. What initial speed (vi) is needed so that when the object is far from Mars, its final speed (vf) is 500 m/s?
Relevant Equations
G = 6.7E-11
Conservation of energy principle: U1 + K1 = U2 + K2
U1 = -GMm/r
K1 = (1/2)mvi^2
U2 = as r approaches infinity, U2 approaches zero
K2 = (1/2)mvf^2

(1/2)mvi^2 - GMm/r = (1/2)mvf^2 + 0

vi = √(vf^2 + (2GMm)/r) = √(250,000 + 2(6.7 E-11)(6 E23)/3400) = 153776.815

But that is not the correct answer, can anybody see my mistake/misunderstanding?
 
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The radius (r) is given in km, isn't it?
 
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Likes berkeman and PeroK
nasu said:
The radius (r) is given in km, isn't it?
omg... converted it to m and fixed it, thank you so much
 

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