a 1000 kg space craft at 500 m/s is on a collision course with a 400 kg satellite travelling at 700 m/s . Their paths are converging at a 45 degree angle . After the collision they remain locked together. What is the final speed of both satellites? What angle is this at

Assume the heavier satellite is traveling in the +x direction. Conserve momentum, so the final velocity (xi+yj) is the solution to

1000*500i + 400*700(.707i+.707j) = (1000+700)(xi+yj)

That will give the x- and y-components of the final velocity, which you can then express as magnitude and direction.

To determine the final speed of both satellites after the collision, we need to apply the principle of conservation of momentum:

1. Start by calculating the momentum of each satellite before the collision. The momentum (p) of an object is defined as the product of its mass (m) and velocity (v): p = m * v.

For the 1000 kg space craft:
Momentum = Mass * Velocity = 1000 kg * 500 m/s = 500,000 kg*m/s

For the 400 kg satellite:
Momentum = Mass * Velocity = 400 kg * 700 m/s = 280,000 kg*m/s

2. Next, add the momentum vectors of both satellites using vector addition. Since their paths are converging at a 45-degree angle, we can resolve their momenta into perpendicular components.

For the 1000 kg space craft:
The momentum vector can be divided into two perpendicular components: one along the direction of motion (500 m/s) and the other perpendicular (at 90 degrees) to the direction of motion. The perpendicular component can be found by multiplying the magnitude of the momentum (500,000 kg*m/s) by the sine of the angle (45 degrees): Perpendicular component = 500,000 kg*m/s * sin(45) = 353,553 kg*m/s.

For the 400 kg satellite:
The momentum vector can also be divided into two perpendicular components: one along the direction of motion (700 m/s) and the other perpendicular (at 90 degrees) to the direction of motion. The perpendicular component can be found by multiplying the magnitude of the momentum (280,000 kg*m/s) by the sine of the angle (45 degrees): Perpendicular component = 280,000 kg*m/s * sin(45) = 198,446 kg*m/s.

3. Since momentum is conserved during the collision, the total momentum before the collision equals the total momentum after the collision:

Total initial momentum = Total final momentum

500,000 kg*m/s + 280,000 kg*m/s = (1000 kg + 400 kg) * final velocity

780,000 kg*m/s = 1400 kg * final velocity

Final velocity = 780,000 kg*m/s / 1400 kg ≈ 557.14 m/s

Hence, the final speed of both satellites after the collision is approximately 557.14 m/s.

4. To find the angle at which the final velocity vector points, we need to apply trigonometry. Since the two satellites remain locked together after the collision, the angle will be the same as the initial angle between their paths (45 degrees).

Therefore, the final angle of their combined velocity vector is also 45 degrees.

In conclusion, the final speed of both satellites after the collision is approximately 557.14 m/s, and the angle of the final velocity vector is 45 degrees.