Motion in a Plane Homework: Thrust Force, Angle & Burn Length

  • Thread starter Thread starter physnoob
  • Start date Start date
  • Tags Tags
    Motion Plane
Click For Summary
SUMMARY

The discussion revolves around a physics homework problem involving a spacecraft's maneuvering to enter a pod using a single rocket burn. The spacecraft has a mass of 20,000 kg and is initially traveling at 2,000 m/s. The required thrust force calculated by the user is 100,600 N, but the textbook states it should be 103,000 N. The user also calculated the angle for the thrust direction to be 23.41 degrees below the positive x-axis, while the textbook indicates 26.6 degrees. The discrepancy suggests a need for reevaluation of the approach, particularly regarding the trajectory and centripetal force considerations.

PREREQUISITES
  • Understanding of Newton's laws of motion
  • Familiarity with kinematic equations, specifically V12 = V02 + 2aS
  • Basic knowledge of thrust force calculations in spacecraft dynamics
  • Concept of centripetal force and its application in circular motion
NEXT STEPS
  • Review the derivation of thrust force in rocket propulsion
  • Study the principles of centripetal acceleration and its relation to spacecraft maneuvers
  • Learn about trajectory calculations for spacecraft entering a gravitational field
  • Explore the use of vector components in analyzing motion in two dimensions
USEFUL FOR

This discussion is beneficial for physics students, aerospace engineering students, and anyone interested in spacecraft dynamics and maneuvering techniques.

physnoob
Messages
15
Reaction score
0

Homework Statement


Driving a spaceship isn't as easy as it looks in the movies. Imagine you're a physics student in the 31st century. You live in a remote space colony where the gravitational force from any stars or planets is negligible. You're on your way home from school, coasting along in your 20,000 kg personal spacecraft at 2 km/s, when the computer alerts you to the fact that the entrance to your pod is 500 km away along a line 30 degrees from your present heading, as shown in the following figure:
http://img130.imageshack.us/img130/4743/knightv.jpg
You need to make a left turn so that you can enter the pod going straight ahead at 1 km/s. You could do this with a series of small rocket burns, but you want to impress the girls in the spacecraft behind you by getting through the entrance with a single rocket burn. You can use small thrusters to quickly rotate your spacecraft to a different orientation before and after the main rocket burn.

You need to determine three things: how to orient your spacecraft for the main rocket burn, the magnitude F-thrust of the rocket burn, and the length of the burn. Use a coordinate system in which you start at the origin and are initially moving aling the x-axis. Measure the orientation of you spacecraft by the angle it makes with the positive x-axis. Your initial orientation is 0 degrees. You can end the burn before you reach the entrance, but you're not allowed to have the engine on as you pass through the entrance. Mass loss during the burn is negligible.

m = 20000kg
Vx0 = 2000 m/s
Vx1 = 0 m/s
Vy0 = 0 m/s
Vy1 = 1000 m/s

Homework Equations



V12 = V02 + 2aS

The Attempt at a Solution


The distance in the x direction is 500000cos(30), the y direction is 500000sin(30).
I use the formula above to solve for the acceleration in the x and y direction, ax = 4.62, ay = 2, so a = \sqrt{4.62^2 + 2^2} = 5.03 m/s/s.
Thrust force = 20000*5.03 = 100600N
Then i use inverse tangent to find the angle, which is 23.41 degrees below positive x-axis (where the thruster should point at).
However, the answer in the book is 103000N and 26.6 degrees below the positive x-axis.
What did i do wrong?
Any help is appreciated!
 
Last edited by a moderator:
Physics news on Phys.org
bump, please help!
 
I think they're implying that you want to turn the corner by following an arc that's a quarter of a circle. You would then have to choose what radius that circle would have. Thruster force would be centripetal force. That's the only idea I have.
 
mikelepore said:
I think they're implying that you want to turn the corner by following an arc that's a quarter of a circle. You would then have to choose what radius that circle would have. Thruster force would be centripetal force. That's the only idea I have.
I don't think that's the case. If i turn the corner by following an arc, i would have to use a series of rocket burns, but the problem is asking to do it with a single rocket burn, and i can use small thrusters to change the angle before i apply the main rocket burn, but I'm not sure though.

Please help! I need to submit this to my teacher by the end of the night!
Any help is greatly appreciated!
Thanks!
 

Similar threads

  • · Replies 16 ·
Replies
16
Views
13K
  • · Replies 37 ·
2
Replies
37
Views
10K
  • · Replies 8 ·
Replies
8
Views
2K
  • · Replies 1 ·
Replies
1
Views
2K
  • · Replies 23 ·
Replies
23
Views
3K
  • · Replies 6 ·
Replies
6
Views
3K
  • · Replies 3 ·
Replies
3
Views
2K
Replies
8
Views
2K
  • · Replies 2 ·
Replies
2
Views
3K
Replies
5
Views
2K