How Does Igniting Fuel at the Trajectory's Apex Affect Missile Debris Dispersal?

In summary: I don't want to give you the answer, but this should be enough that you can solve for the time of flight and the distance to the bunker for each piece.
  • #1
gettix
1
0

Homework Statement


In testing a missile defense system, a missile is red from the ground on a
trajectory that would directly hit a bunker some distance away. When the missile is
at the top of the trajectory, a laser light from the bunker ignites fuel in the missile
and the missile disintegrates into two pieces, one twice as massive as the other. The
pieces reach the ground nearly simultaneously, 60m apart from each other.

(a) By how much does the larger piece miss the bunker? Hint: Consider motion of
the center of mass.
(b) By how much does the smaller piece miss the bunker?
(c) How important is the information that the fuel ignited at the top of the trajectory?

Homework Equations



The Attempt at a Solution




so far I figured out this:
http://imgur.com/MdLrl
http://imgur.com/YqBet

I know that I need one more equation to get all the unknowns.
the homework is due in 5 hours if anyone could help I would love you forever.
 
Physics news on Phys.org
  • #2
This looks like a conservation of momentum problem, more than a kinematics problem.

For part (c), the rocket is tangent to the x-axis (i.e., going horizontally) when the laser zaps it, so there should be no change in the y components of the velocity or the acceleration when it blows. Both pieces should have the same velocity and acceleration in that dimension. At max height, the y component of velocity is zero, so all of the momentum is in the x direction.

If we use your definition of the initial mass as 3m and the two pieces as m and 2m, and define the initial velocity as v0, then conservation of momentum is

p0 = p1 + p2

where

p0 = m0v0 = (3m)v0

Let's define the change in velocity of the small piece as v1 and the change in velocity of the larger piece as v2. This is a bit different than the usual notation, but there's a method to my madness.

Define (v0 + v1) as the velocity of the small piece and (v0 + v2) as the velocity of the big piece. v1 and v2 are the changes in velocity from the fuel exploding. Intuitively, one of these should be the opposite of the other as they fly apart, but let's leave the signs as positive for now.

So, p1 = m (v0 + v1) and p2 = 2m (v0 + v2)

The conservation law is then p0 = p1 + p2 or

3m(v0) = m (v0 + v1) + 2m (v0 + v2)

Multiply it out:

3m(v0) = m(v0) + m(v1) + 2m(v0) + 2m(v2)

Collect similar terms:

3m(v0) = 3m(v0) + m(v1) + 2m(v2)

Subtract 3m(v0) from both sides:

0 = m(v1) + 2m(v2)

Divide by m:

0 = v1 + 2(v2)

Subtract 2(v2) from both sides

- 2(v2) = v1, or v1 = -2(v2)

So, intuition and our signs match up. The little piece's change in velocity is opposite in direction to the big one and its velocity changes twice as much as the big piece changes.

That should be a big enough hint for you.
 
Last edited:

1. What factors affect the trajectory of a missile?

The trajectory of a missile is affected by several factors, including the initial launch velocity, the angle at which the missile is launched, air resistance, and the force of gravity. Other factors such as wind speed and direction, temperature, and altitude can also play a role.

2. How do engineers calculate the trajectory of a missile?

Engineers use mathematical equations and computer programs to calculate the trajectory of a missile. These calculations take into account the initial conditions of the launch, as well as the environmental factors that may affect the missile's flight path.

3. What is the difference between a ballistic and guided missile trajectory?

A ballistic trajectory is a free-falling path that is determined solely by the initial conditions and the forces acting on the missile. On the other hand, a guided missile trajectory is controlled by an onboard guidance system that can adjust the flight path to reach a specific target.

4. Can a missile's trajectory be changed mid-flight?

Yes, some missiles have the capability to change their trajectory during flight. This is achieved through the use of guidance systems, which can make small adjustments to the missile's fins or thrust to alter its flight path.

5. What are the potential challenges in predicting the trajectory of a missile?

Predicting the trajectory of a missile can be challenging due to the complex nature of the flight path. Factors such as wind, air resistance, and gravity can all affect the missile's trajectory, and slight variations in these factors can lead to significant changes in the flight path. Additionally, unpredictable events such as malfunctions or unexpected environmental conditions can also impact the trajectory of a missile.

Similar threads

  • Introductory Physics Homework Help
Replies
1
Views
7K
  • Introductory Physics Homework Help
Replies
7
Views
1K
  • Introductory Physics Homework Help
Replies
22
Views
3K
  • Introductory Physics Homework Help
Replies
2
Views
1K
  • Introductory Physics Homework Help
Replies
4
Views
2K
  • Introductory Physics Homework Help
Replies
13
Views
2K
  • Introductory Physics Homework Help
3
Replies
70
Views
6K
  • Introductory Physics Homework Help
Replies
2
Views
5K
  • Introductory Physics Homework Help
Replies
7
Views
2K
  • Introductory Physics Homework Help
Replies
7
Views
8K
Back
Top