A 33300 lb (earth weight) rocket in outer space has two constant forces acting upon it,

F1 = (-166i + 392j) lb and
F2 = (50i + -54j) lb.
Its initial velocity is (39i + 64j) ft/s.
How far is it from where it started after 33 seconds?

The net force is F1 + F2 = -116 i + 338 j

In the x direction, the final location is changed by 39*33 + (1/2)(-116/33,300)*33^2

There is a similar equation for the change in the y coordinate: Voy*t + (1/2)(Fy/m)t^2

Thanks for the timely help.

To find the distance the rocket has traveled after 33 seconds, we need to calculate its final position. We can do this by integrating the velocity vector over the given time interval.

Given:
Initial velocity (u) = (39i + 64j) ft/s
Time (t) = 33 seconds

Step 1: Calculate the acceleration vector (a) using the given forces.
To find the acceleration vector, we can use Newton's second law, which states that F = ma, where F is the net force acting on the object and a is the acceleration vector.
Since we have two constant forces acting on the rocket, we can add them to get the net force.

Given forces:
F1 = (-166i + 392j) lb
F2 = (50i + -54j) lb

Net force (F) = F1 + F2
= (-166i + 392j) lb + (50i + -54j) lb
= (-116i + 338j) lb

Since the rocket's weight is given in pounds, we can convert it to mass (in slugs) using the conversion factor 1 slug = 32.174 lb.

Mass of the rocket (m) = 33300 lb / 32.174 lb/slug
≈ 1032.35 slugs

Now, we can calculate the acceleration (a) using F = ma:
a = F / m
= (-116i + 338j) lb / 1032.35 slugs

Step 2: Integrate the acceleration vector to find the final velocity.
To find the final velocity, we need to integrate the acceleration vector over time.
Using the initial velocity (u) and the acceleration (a) obtained in step 1, we can use the following equation:

Final velocity (v) = u + at

Since the mass of the rocket is constant, the change in velocity is simply a linear function of time.

Final velocity (v) = (39i + 64j) ft/s + [(-116i + 338j) lb / 1032.35 slugs] * 33 seconds

Step 3: Calculate the displacement vector using the trapezoidal rule.
To find the displacement vector, we need to integrate the velocity vector over time using the trapezoidal rule.
The trapezoidal rule approximates the integral by dividing the time interval into small subintervals and approximating each subinterval using the average of the velocities at the beginning and end of the subinterval.

Displacement vector (s) = ∫v dt
≈ ∑[(v(t + Δt) + v(t)) / 2] * Δt

Here, we can choose a small time interval, like Δt = 0.1 seconds, and sum up the products of the average velocities and time intervals for each subinterval.

s = ∑[(v(t + Δt) + v(t)) / 2] * Δt = ∑[(v(t) + v(t + Δt)) / 2] * Δt

Starting from t = 0 seconds, we can iterate the integration formula for each Δt until we reach t = 33 seconds.

Step 4: Calculate the magnitude of the displacement vector.
Finally, we can calculate the magnitude of the displacement vector using the Pythagorean theorem:

Magnitude of displacement vector (|s|) = √(s_x^2 + s_y^2)

By following these steps, we can determine the distance the rocket has traveled from where it started after 33 seconds.