Step 1: Using the formula for gravitational acceleration at altitude.
The acceleration due to gravity at a height \( h \) above the Earth's surface is given by:
\[
g' = g \left( \frac{R}{R + h} \right)^2
\]
where:
\( g \) is the acceleration due to gravity at the surface,
\( R \) is the radius of the Earth, and
\( h \) is the height above the Earth's surface.
Step 2: Calculating the ratio \( \frac{g'}{g} \).
The ratio \( \frac{g'}{g} \) is:
\[
\frac{g'}{g} = \left( \frac{R}{R + h} \right)^2
\]
Substituting the given values:
\( R = 6370 \, {km} \),
\( h = 50 \, {km} \),
we get:
\[
\frac{g'}{g} = \left( \frac{6370}{6370 + 50} \right)^2 = \left( \frac{6370}{6420} \right)^2
\]
Step 3: Simplifying the expression.
First, calculate the ratio inside the parentheses:
\[
\frac{6370}{6420} \approx 0.991 \quad \Rightarrow \quad \left( 0.991 \right)^2 \approx 0.982
\]
Thus, the ratio of \( g' \) to \( g \) is approximately:
\[
\frac{g'}{g} \approx 0.98
\]