How to Calculate the Flight Time and Apex for a Model Rocket Launch in Excel?

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SUMMARY

The discussion focuses on calculating the flight time and apex of a model rocket using Excel, with specific parameters including a mass of 0.05 kg, an initial force of 16 N, and gravitational acceleration of 9.81 m/s². The calculations are divided into three stages: the first stage involves a thrust phase lasting 0.15 seconds, resulting in a velocity of 46.53 m/s and a height of 10.47 m. The second stage, lasting until 6.15 seconds, requires reevaluation of the velocity due to gravity's downward force, leading to a height of 111.11 m. The discussion highlights the need for clarity in calculating total flight time and apex, emphasizing the correct application of gravitational acceleration.

PREREQUISITES
  • Understanding of Newton's second law of motion (ΣF = ma)
  • Basic knowledge of kinematic equations (v(t) = vo + at, h(t) = ho + vo + 0.5at²)
  • Familiarity with Excel for plotting and calculations
  • Concept of projectile motion and forces acting on an object
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  • Learn how to implement kinematic equations in Excel for real-time calculations
  • Research the effects of drag and other forces on model rocket flight
  • Explore advanced Excel functions for data visualization and plotting
  • Study the principles of model rocket design and performance optimization
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radarspec
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A brief explanation, this assignment is to be done in Excel and also has to be turned in with handwritten solutions for finding total flight time and apex. If I can get the handwritten part done Excel is a piece of cake.

Homework Statement


A model rocket is launched and I am to evaluate the 3 stages it goes through. During the first 0.15s the rocket (m=0.05 kg) is launched with a force of 16N. It then coasts upward while being slowed done by gravity (g=9.81m/s2. After it reaches apex(max altitude it starts to fall back down. It also deploys a parachute 6 sec. after the motor stops with a constant speed of 10 m/s until it hits ground. Calculate the speed and altitude of the rocket over it's flight time and plot them.

Knowns:
g=9.81m/s2
FE=16N
m=0.05 kg
vo=0m/s
\Deltat=0.01s

Unknowns:
acceleration
velocity
height
total time

Homework Equations


\SigmaF=ma
v(t)=vo+at
h(t)=ho+vo+.5at2

The Attempt at a Solution



Stage 1: 0\leq t \leq 0.15s
use dt=0.01s (was told to do this by teacher for stage 1)
\SigmaF=ma
Fe-w=may
ay=\frac{Fe-w}{m}
ay=\frac{16N-(0.05)(9.81)}{0.05}=310.19m/s2

v=vo+at
v=0+(310.19)(0.15)=46.53m/s

h=ho+v0+.5at2
h=.5at2
h=.5(310.19)(0.15)2
h=10.47 m

Stage 2: 0.15 \leq t \leq 6.15s
\SigmaF=ma
-w=may
ay=-g

v=vo+at
v=46.53+(9.81)(6.15)=106.86m/s

h=10.47m+(46.53)(6.15)+.5(-9.81)(6.15)2=111.11m

Stage 3: 6.15 \leq t \leq total time

Stage 3 is were I get lost could some point me in the right direction as to find total time and apex.
 
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Your stage 2 is incorrect. At the end of stage 1, you have the rocket's velocity as 46.53 m/s upwards (correct). Then at the end of stage 2, during which the only force is gravity (downward), you have the rocket's velocity as 106.86 m/s upwards. Ask yourself, does this make any sense?
 
So I would be using -9.81 instead of 9.81 for gravity now? Also would apex be the addition of the height of stage 1 & 2 added together. 111.11 + 10.47 = 121.58m?

Also the velocity and height numbers seem small given the acceleration at lift off.
 
Last edited:

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