The atmospheric pressure at sea level is about 101 kilopascals. For every 1000-m increase in altitude, the pressure decreases about 11.5%. What is the pressure at an altitude of 5000 m?

Let's start by finding the decrease in pressure for every 1000-m increase in altitude. We know that the pressure decreases by 11.5% for every 1000-m increase.

So the pressure decreases by 11.5/100 * 101 kPa = 11.65 kPa for every 1000-m increase.

To find the pressure at an altitude of 5000 m, we need to multiply the decrease in pressure by the number of 1000-m increases. Since we have 5 increments of 1000 m, we can multiply the decrease in pressure by 5.

Therefore, the pressure at an altitude of 5000 m is 5 * 11.65 kPa = 58.25 kPa. Answer: \boxed{58.25}.

To find the pressure at an altitude of 5000 m, we need to calculate the decrease in pressure for every 1000-m increase in altitude.

First, let's calculate the decrease in pressure for 1000 m:
11.5% of 101 kilopascals is (11.5/100) * 101 = 11.665 kilopascals.

Next, we can calculate the decrease in pressure for 5000 m:
Since 5000 m is 5 times 1000 m, the decrease in pressure would be 5 * 11.665 kilopascals = 58.325 kilopascals.

Finally, we can calculate the pressure at an altitude of 5000 m:
101 kilopascals - 58.325 kilopascals = 42.675 kilopascals.

Therefore, the pressure at an altitude of 5000 m is about 42.675 kilopascals.

To calculate the pressure at an altitude of 5000 m, we need to use the given information:

1. The atmospheric pressure at sea level is about 101 kilopascals (kPa).

2. For every 1000 m increase in altitude, the pressure decreases about 11.5%.

First, let's determine how many 1000 m increments are there in 5000 m.

5000 m ÷ 1000 m = 5

Therefore, there are 5 increments of 1000 m in 5000 m.

Next, we need to calculate the total decrease in pressure for 5 increments.

11.5% decrease x 5 increments = 57.5% decrease

To find the remaining pressure, we subtract the decrease from the initial pressure.

Remaining pressure = Initial pressure - Decrease
= 101 kPa - (57.5% of 101 kPa)

To calculate the decrease in pressure, we multiply 57.5% by 101 kPa.

Decrease = (57.5/100) x 101 kPa
= 0.575 x 101 kPa
= 58.075 kPa

Finally, we can calculate the remaining pressure at an altitude of 5000 m:

Remaining pressure = 101 kPa - 58.075 kPa
= 42.925 kPa

Therefore, the pressure at an altitude of 5000 m is approximately 42.925 kilopascals.