How Do You Calculate Time of Flight and Range for a Rocket Launched at an Angle?

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Homework Help Overview

The discussion revolves around calculating the time of flight and horizontal range for a rocket launched at an angle of 36.87º with a specified acceleration and duration of thrust. Participants are examining the implications of the rocket's trajectory and the effects of gravity during its flight.

Discussion Character

  • Exploratory, Assumption checking, Problem interpretation

Approaches and Questions Raised

  • Participants discuss the initial calculations regarding distance and velocity during the rocket's powered ascent. Some question the interpretation of the rocket's path during the first 20 seconds, considering whether it follows a straight line due to constant acceleration.

Discussion Status

There is an ongoing exploration of different interpretations of the problem, particularly regarding the angle of launch and the effects of gravity. Some participants have offered insights into the nature of the rocket's motion, while others have identified potential errors in the original calculations.

Contextual Notes

Participants note ambiguity in the problem statement, particularly concerning the role of gravity during the initial acceleration phase. There is also a mention of the need for clarity regarding the rocket's trajectory and whether it is treated as a straight line or follows a more complex path.

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Homework Statement


A rocket is launched at an angle of 36.87º (sin=0.6 cos=0.8) with an acceleration of 30m/s² for 20s (fuel runs out). Find a) total time of flight b) horizontal range.

Homework Equations

The Attempt at a Solution


for the first 20 seconds:
v= 30 * 20 = 600m/s d=30 * 20² * 0.5 = 6000m
so vertical distance is= 6000 * 0.6 = 3600m
and horizontal distance is= 6000 * 0.8 = 4800m

fuel runs out
vertical speed is v= 600 * 0.6 = 360m/s
0 = 360 - 10*t .: t=36s (time to reach max height)
max height is= 3600 + 360*36 - 10*36²*0.5 = 10,080m

after reaching max height
10080 = 10 * t² * 0.5 .: t=45s (time to land)
t=36+45=81s (amount of time gravity is doing it's job to make it fall)
horizontal speed is v= 600*0.8 = 480m/s
horizontal distance = 480 * 81 = 38880m

total horizontal distance = 4800 + 38880 = 43680m
total time of flight = 20 + 81 = 101sWell, it's wrong. The answer should be 41,4km and 125s.
Help me please, thanks in advance.
 
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125 seconds seems to match with 36.87 degrees off of vertical rather than horizontal.
Try the calculations using 0 degrees as vertical.
 
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HueHue said:
for the first 20 seconds:
v= 30 * 20 = 600m/s d=30 * 20² * 0.5 = 6000m
so vertical distance is= 6000 * 0.6 = 3600m
and horizontal distance is= 6000 * 0.8 = 4800m
This is saying that its path for the first 20 secs will be a straight line??
 
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Since acceleration is given and not thrust, it sounds like this is a straight line simplified problem.
 
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Thanks everyone, I figured out what's wrong. I swaped the 0.6's with the 0.8's
Now I'm getting the right results!
Thanks again, see ya
 
The problem statement is a bit ambiguous in terms of gravity for the first 20 seconds, but as you get the correct result you chose the intended interpretation apparently.

NascentOxygen said:
This is saying that its path for the first 20 secs will be a straight line??
Every rocket accelerating from rest will move in a straight line if the direction and magnitude of thrust does not change - constant acceleration from rest gives a straight line.
 
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mfb said:
Every rocket accelerating from rest will move in a straight line if the direction and magnitude of thrust does not change
Indeed, and for fireworks rockets that direction is fixed as "straight out the back" and they invariably follow an arc across the sky. Practically every rocket we observe launched at a low angle does not follow a straight line.

The question could be improved, perhaps by changing to 'a guided missile', so the reader is made aware it is steerable.
 
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NascentOxygen said:
Practically every rocket we observe launched at a low angle does not follow a straight line.
Usually because thrust or the orientation of the rocket change (e.g. firework rockets have a short acceleration phase and then fly under the influence of gravity), but here the direction and magnitude is fixed, so the rocket follows a straight line until it runs out of fuel.
 
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