HPR Level 2 Technical Questions

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#1. The center of pressure (CP) of a rocket is generally defined as:

#2. Which describes the thrust curve of a regressive motor burn?

#3. What happens to the coefficient of drag (Cd) as the rocket approaches the speed of sound?

#4. What is the major issue with accelerometer-based altimeters?

#5. What are the three forces acting upon a rocket during flight?

#6. What effect does a boat tail have on a subsonic rocket’s coefficient of drag (C d)?

#7. Which of the motors listed below has the highest total impulse?

#8. What is the purpose of a launch rod, rail or tower?

#9. The average thrust of a rocket motor is 100 Newtons, and the burn time is 4 seconds. What is the total impulse?

#10. What are three methods used to shift the center of pressure (CP) aft?

#11. What is the purpose of a launch lug or rail buttons?

#12. How can a statically unstable rocket be made stable?

#13. In general terms, the total impulse of a rocket motor can be described as:

#14. What ordinarily happens to the center of gravity (CG) of a rocket during a solid rocket motor’s thrusting phase?

#15. Which of the motors listed below has the highest average thrust?

#16. The flight of a high-power rocket can be separated into three portions; they are:

#17. What is the primary requirement for a rocket motor ignitor?

#18. What can happen if all the motors of a cluster do not ignite at launch?

#19. What is a Newton?

#20. Which describes the thrust curve of a progressive motor?

#21. What are three methods used to shift the center of gravity (CG) of a rocket forward?

#22. What is a Cato?

#23. For an inherently stable rocket, which statement about the center of gravity (CG) and the center of pressure (CP) is true?

#24. What is the most common oxidizer in commercially available high power composite solid rocket motors?

#25. Rocket A is descending at 10 feet per second, rocket B weighs the same but is descending at 20 feet per second. Which statement is true?

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