Can't figure out solution -- Space probe with engine thrust vectors

In summary: I'll be back later tonight...I'm not sure what you mean. If you have a right triangle with two sides of length 1, what is the length of the hypotenuse?I have to bail for a couple... but I'll be back later tonight...As a summary, in the given conversation, the problem of calculating the time it would take for a space probe to travel a certain distance when fired with perpendicular forces was discussed. By using the Pythagorean theorem and the equation D=V0t+1/2at^2, it was determined that the time would be equal to the ratio of the magnitude of the force in the first and second cases. It was also clarified that the magnitude of the
  • #1
Ben5386
13
1

Homework Statement


A space probe has two engines. Each generates the same amount of force when fired, and the directions of these forces can be independently adjusted. When the engines are fired simultaneously and each applies its force in the same direction, the probe, starting from rest, takes 25 s to travel a certain distance. How long does it take to travel the same distance, again starting from rest, if the engines are fired simultaneously and the forces that they apply to the probe are perpendicular?
V0=0
t1=25

Homework Equations


D=V0t+1/2at^2
a=2T/m

The Attempt at a Solution


D= 0*t+1/2(2T/m)*25^2
D=(T/m)*25^2




 
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  • #2
Ben5386 said:

Homework Statement


A space probe has two engines. Each generates the same amount of force when fired, and the directions of these forces can be independently adjusted. When the engines are fired simultaneously and each applies its force in the same direction, the probe, starting from rest, takes 25 s to travel a certain distance. How long does it take to travel the same distance, again starting from rest, if the engines are fired simultaneously and the forces that they apply to the probe are perpendicular?
V0=0
t1=25

Homework Equations


D=V0t+1/2at^2
a=2T/m

3. The Attempt at a Solution

D= 0*t+1/2(2T/m)*25^2
D=(T/m)*25^2
Welcome to the PF.

You will need to use vectors to figure this out (or at least express the thrusts and distances in two dimensions). Can you draw two diagrams for the vector thrusts involved?
 
  • #3
berkeman said:
Welcome to the PF.

You will need to use vectors to figure this out (or at least express the thrusts and distances in two dimensions). Can you draw two diagrams for the vector thrusts involved?
How do I draw the force vectors on this site I have them on paper
 
  • #4
If you can take a good picture of them (clear, bright, not fuzzy, etc.), you can use the UPLOAD button in the reply window to upload a JPG file from your PC or laptop. :smile:
 
  • #5
berkeman said:
If you can take a good picture of them (clear, bright, not fuzzy, etc.), you can use the UPLOAD button in the reply window to upload a JPG file from your PC or laptop. :smile:
Here they are the upside down T is the perpendicular vector with the F in the middle and parallel are the ones are below.
 

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  • #6
Ben5386 said:
Here they are the upside down T is the perpendicular vector with the F in the middle and parallel are the ones are below.
So what is the magnitude of the resultant force for the 2nd case? What is the ratio of the forces for the first and second case? What equation would you then use to figure out the ratio of the times it takes to travel a certain distance?
 
  • #7
berkeman said:
So what is the magnitude of the resultant force for the 2nd case? What is the ratio of the forces for the first and second case? What equation would you then use to figure out the ratio of the times it takes to travel a certain distance?
I think it is pythagorean theorem for the magnitude of the resultant force of the second case. To solve for the distance I would use the equation D=Vo+1/2at^2 and since the distance is the same I can plug in the distance for the second case
 
  • #8
Ben5386 said:
I think it is pythagorean theorem for the magnitude of the resultant force of the second case. To solve for the distance I would use the equation D=Vo+1/2at^2 and since the distance is the same I can plug in the distance for the second case
You are on the right track. Use the fact that Vo=0 to help simplify that equation, so you can take ratios.

Also, on your diagram, re-label the right-angle drawing with each of the two right-angle forces being "F", and the middle resultant will then be what by the Pythagorean theorem?
 
  • #9
berkeman said:
You are on the right track. Use the fact that Vo=0 to help simplify that equation, so you can take ratios.

Also, on your diagram, re-label the right-angle drawing with each of the two right-angle forces being "F", and the middle resultant will then be what by the Pythagorean theorem?
The Magnitude of the vector in the middle labeled M in the picture
 

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  • #10
Ben5386 said:
The Magnitude of the vector in the middle labeled M in the picture
So in the first case, M=2F. What is M in the second case? What does that give you for the ratio of the two times to go the same distance? What does that give you for the 2nd time? You're almost done! :smile:
 
  • #11
I have D=1/2(2T/m)*t^2 which reduces down to D=(F/m)*t^2 and for the second case is M equal to F?
 
  • #12
berkeman said:
So in the first case, M=2F. What is M in the second case? What does that give you for the ratio of the two times to go the same distance? What does that give you for the 2nd time? You're almost done! :smile:
I have D=1/2(2T/m)*t^2 which reduces down to D=(F/m)*t^2 and for the second case is M equal to F?
 
  • #13
Ben5386 said:
I have D=1/2(2T/m)*t^2 which reduces down to D=(F/m)*t^2 and for the second case is M equal to F?
No, M for the second case is not F. It is more than F and less than 2F. Look at your diagram and use the square you drew with F as each side and M on the diagonal (hypotenuse of the 2 triangles...).
 
  • #14
berkeman said:
No, M for the second case is not F. It is more than F and less than 2F. Look at your diagram and use the square you drew with F as each side and M on the diagonal (hypotenuse of the 2 triangles...).
Would it be F/M meaning the cosine of 45 degrees
 
  • #15
Ben5386 said:
Would it be F/M meaning the cosine of 45 degrees
I'm not sure what you mean.

If you have a right triangle with two sides of length 1, what is the length of the hypotenuse?

I have to bail for a couple of hours. You are very close to solving this. I'll check back in later tonight to be sure you got the right answer. :smile:
 
  • #16
berkeman said:
I'm not sure what you mean.

If you have a right triangle with two sides of length 1, what is the length of the hypotenuse?

I have to bail for a couple of hours. You are very close to solving this. I'll check back in later tonight to be sure you got the right answer. :smile:
Would it be the square root of 2F
 
  • #17
Ben5386 said:
Would it be the square root of 2F
Written more precisely, yes it would be F√2.

So finish it off now (if you haven't already). What is the ratio of the times? What is the time for the second scenario?
 
  • #18
berkeman said:
Written more precisely, yes it would be F√2.

So finish it off now (if you haven't already). What is the ratio of the times? What is the time for the second scenario?
I know that this answer is probably wrong but is it 84.089
 
  • #19
Ben5386 said:
I know that this answer is probably wrong but is it 84.089
Please don't make me do extra work :smile: Please show your detailed work with units included. Thanks.
 
  • #20
I have the ratio of the two and I have 2F/F
berkeman said:
Please don't make me do extra work :smile: Please show your detailed work with units included. Thanks.
I have the ratio of 2F/F(sqrt(2)) which reduces to the sqrt(2) sorry my computer doesn't show me the mathematical functions. so I put in what I got for distance earlier which is (F/m)*t^2=1/2*sqrt(2)*t^2
 
  • #21
Ben5386 said:
I have the ratio of the two and I have 2F/F

I have the ratio of 2F/F(sqrt(2)) which reduces to the sqrt(2) sorry my computer doesn't show me the mathematical functions. so I put in what I got for distance earlier which is (F/m)*t^2=1/2*sqrt(2)*t^2
That doesn't help. Show your work with units included.
 
  • #22
berkeman said:
That doesn't help. Show your work with units included.
I don't know how but I got it the answer is 29.73 seconds.
 
  • #23
Ben5386 said:
I don't know how but I got it the answer is 29.73 seconds.
Thanks so much for your help :)
 
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1. How do engine thrust vectors affect the trajectory of a space probe?

Engine thrust vectors play a crucial role in determining the direction and speed of a space probe. By adjusting the angle and intensity of the thrust, scientists can control the path of the probe and guide it towards its destination.

2. What factors can affect the accuracy of calculating engine thrust vectors?

Several factors can impact the accuracy of calculating engine thrust vectors, including the weight and mass distribution of the space probe, external forces such as gravity and solar wind, and the precision of the thrusters themselves.

3. How can scientists determine the optimal engine thrust vector for a space probe?

Determining the optimal engine thrust vector involves complex calculations and simulations based on the probe's intended trajectory, external forces, and the capabilities of the thrusters. Scientists also take into account variables such as fuel consumption and propulsion limitations to find the most efficient solution.

4. What challenges do scientists face when trying to adjust engine thrust vectors mid-flight?

Adjusting engine thrust vectors during a space probe's flight can be challenging due to the limited communication and control over the probe's position and orientation. Scientists must also consider the potential risks and consequences of making changes to the probe's trajectory in an unpredictable environment.

5. Can engine thrust vectors be used to change the course of a space probe in case of emergency?

Yes, engine thrust vectors can be used in emergency situations to alter the course of a space probe. However, this must be done carefully to avoid causing further complications or damage to the probe. Scientists must also consider the available fuel and the probe's capabilities before making any adjustments.

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