To do this problem, consider what happens in the x-direction (horizontal) and what happens in the y-direction (vertical) as separate things.
a) Calculate displacement in the x-direction for the constant acceleration (of 50 m/s2) using:
x(t) = (1/2)axt2 + vi-xt + x0 where ax = 50.0 m/s2, vi-x = 0 m/s since we are calculating displacement relative to the plane and the rocket is initially traveling at the same speed as the plane, x0 = 0 meters since we are calculating displacement from the initial firing position and calling that initial firing position our "zero" position, and t = 10 s.
b) Calculate displacement in the y-direction for the constant acceleration (of -9.8 m/s2) using:
y(t) = (1/2)ayt2 + vi-yt + y0 where ay = -9.80 m/s2, vi-y = 0 m/s since there is no vertical motion initially, y0 = 0 meters since we are calculating displacement from the initial firing position and calling that initial firing position our "zero" position, and t = 10 s.
c) Total displacement is calculated using the Pythagorean Theorem: d = √(x2 + y2) where "x" is the distance calculated in "a)" and "y" is the distance calculated in "b)".
d) Calculate the velocity in the x-direction from:
vx-f = axt + vi-x where vx-f is the final velocity (after 10 seconds) in the x-direction, ax is again 50.0 m/s2, t = 10.0 s, and vi-x is again 0 m/s (since again we are measuring relative to the aircraft).
Calculate the velocity in the y-direction from:
vy-f = ayt + vi-y where vy-f is the final velocity (after 10 seconds) in the y-direction, ay is again -9.80 m/s2, t = 10.0 s, and vi-y is again 0 m/s (since again there is no initial vertical velocity).
Then combine the vx-f and vy-f into a single velocity magnitude using the Pythagorean Theorem: vf = √(vx-f2 + vy-f2)
e) Using the vx-f and vy-f from "d)", calculate the direction using the trig tangent ratio:
θ = tan-1( vy-f/vx-f)
f) and g) Add 200 m/s to vx-f that was calculated in "d)" and redo the magnitude and direction calculations you did above.