Travis S. Taylor 52
7.10 Use a computer program (such as Mathcad) to graph the critical pressure of the
rocket in Exercises 7.8 and 7.9 versus a wall thickness ranging from 1 to 50 mm.
Also, plot the mass of the rocket versus the wall thickness.
7.11 Use the Mathcad algorithm/code given in Section 7.2 to reanalyze Design
Reference Mission #2 but this time with a 300 kg payload. Note: feel free to
convert the Mathcad code to Matlab or any other software you prefer.
7.12 In Exercise 2.8 we studied the following rocket:
A rocket is launched with a burnout velocity of 75 m/sec, burnout altitude of 300
m, and a burnout range of 100 m. Assuming a flight path angle of 75°, calculate the
final range of the rocket when it impacts the ground.
Use OpenRocket to simulate as best you can the rocket in this Exercise. Simulate
and Plot your results.