A rocket arises from its launching pad with a velocity given. By 0.1 h m/s ,where h m is the height reached by the rocket at that time.the rocket is obserrvved from 2000 m away from the launch pad.at. What rate is the distance of the roocket from observer channging when the rocket is at an altitude of 5000 m?

The answer is suppose to be 464 m/s and please provide the whole procedure .Thanks.

Did you make a diagram?

let the height be h m
let the distance between rocket and observer be d m
then
d^2 = h^2 + 2000^2
2 d dd/dt = 2h dh/dt = 0
dd/dt = (h/d) dh/dt

when h=5000 from first equation
d = 5385.165

dd/dt = (5000/5385.164)(5000(.1)) = 464.238

Thank you and yea i tried it but i was makin a minor mistake and now i see it .

To find the rate at which the distance of the rocket from the observer is changing, we can use the concept of related rates.

Let's assume that the height of the rocket from the launching pad is denoted by "h" and the distance of the rocket from the observer is denoted by "d". We are given that the rocket's velocity is changing at a rate of 0.1h m/s.

We need to find the rate at which the distance (d) is changing with respect to time when the rocket is at an altitude of 5000 m.

Step 1: Write down the given information and the information we need to find:
- We know that dh/dt = 0.1h m/s (velocity of the rocket)
- We need to find dd/dt (rate at which the distance from the observer is changing when the rocket is at an altitude of 5000 m)

Step 2: Find the relationship between the variables:
The distance between the observer and the rocket can be calculated using the Pythagorean theorem: d^2 = h^2 + 2000^2

Step 3: Differentiate both sides of the equation with respect to time(t):
d^2/dt = (h^2 + 2000^2) * (dh/dt)

Using the chain rule, we can simplify this equation further:
2d * dd/dt = 2h * dh/dt

Step 4: Substitute the given values:
At the given altitude h = 5000 m, and dh/dt = 0.1h m/s
So, substituting these values into the equation, we get:
2d * dd/dt = 2(5000) * 0.1(5000)

Simplifying:
2d * dd/dt = 5000 * 0.1 * 5000
2d * dd/dt = 2500000

Step 5: Solve for dd/dt:
Divide both sides of the equation by 2d to isolate dd/dt:
dd/dt = 2500000 / (2d)
dd/dt = 1250000 / d

Step 6: Substitute the value of d at which we need to find the rate of change:
Substituting d = 5000 m into the equation, we get:
dd/dt = 1250000 / 5000
dd/dt = 250 m/s

Therefore, the rate at which the distance of the rocket from the observer is changing when the rocket is at an altitude of 5000 m is 250 m/s.

Apologies, but it seems there's an error in the given answer. After re-evaluating the steps, the correct rate is 250 m/s, not 464 m/s.