Model - predict - do - measure - compare

1. Pre-flight

1.1. Prepare your rocket

  • Launch rod guide tube installed.

  • Loosely pack wadding tissue then streamer.

  • Nose cone stays in but can be pushed out by the ejection charge. May need tape or sanding to adjust.

  • Install A8-3 engine. Should be a friction fit tighter than the nose cone. Likely needs Scotch tape to adjust.

  • Install the igniter. Watch YT: Installing Estes Igniters Without Pain or Disappointment

  • Weigh your ready-to-fly rocket and record the value.

1.2. Pre-flight data

(g) - Your rocket’s mass.

(g) - Propellant mass of the A8-3 motor from your handout.

(s) - Motor burn time.

(mm) - Rocket body diameter. For reference, the A8-3 motor itself is 18 mm diameter.

(no units) - Cd drag coefficient estimate. Read "Choosing the right drag coefficient".

1.3. Flight prediction

Go to https://www.altimetercloud.com/tools/altitude_prediction/ - Model Rocket Altitude Predictor

  • Select the "Estes Industries / A8" motor.

  • Fill in your rocket’s other information.

240 m - Launch site altitude.

(m/s) / (mph) - Max velocity

(s) - Coast time

(s) - Launch-to-apogee time

(m) / (ft) - Predicted apogee (max height)

1.4. Launch!

two station tracking

(ft) - Pad to A distance

(ft) - Pad to B distance

(degrees) - max angle A

(degrees) - max angle B

1.5. Analysis

(g) - Post-fight rocket mass. (difference should be the propellant and ejection charge)

Use the provided spreadsheet to compute the apogee:

(m) / (ft) - Computed apogee.

estes rocket engine operation

For way better predictions and rocket design: