This table contains information about the most common causes for a rocket to fail.
The intent is that, with proper care and prevention, these failure modes may be avoided. (Source From NASA Houston Rocket Club NAR Section 365)
TASK/STEP | HAZARD | CAUSE | PREVENTATIVE MEASURE |
Any | 1. Non-Hazardous Anomaly | Premature parachute ejection | All flights in this category result in safe landing under parachute. – |
Flight preparations | 2. Premature motor ignition | Connecting igniter to live ignition system | – Using systems with a switch that returns to “off” when released per NAR safety code. Ensure continuity checker is igniter/electric match/flash bulb safe. |
3. Premature ejection charge ignition | Electronic Altimeter failure / capacitor discharge | -use switch or shunt on charge circuits until placed on pad | |
Rocket boost | 4. Erratic boost | a. Rocket unstable | – Check the stability of the rocket with the selected motor per NAR safety code if not a proven design/motor combination -Use computer CG/CP program, CP should be 1.0 body diameter aft of CG |
b. Unstable launch pad | – insure launch pad is sufficiently strong to withstand wind and launch forces. – use rail system for HPR launches | ||
c. Too much wind | – Launch only in winds of less than 20 mph as required by NAR safety code – In windy conditions low thrust launches should be avoided. | ||
d. Insufficient thrust | – Follow anufacturer¹s recommended maximum lift-off weight per NAR safety code – Use computer simulation program to determine thrust required | ||
5. Airframe failure | a. Improper construction | – Follow manufacturer assembly instructions. – On original designs use standard construction methods. – Check for secure fins, launch lugs, and proper nose cone fit. – Check secure motor mount assembly. | |
b. Fin flutter | – Be sure to align grain with leading edge of fin. (standard construction method) – Avoid high aspect ratio fins | ||
c. Improper Motor Selection | – Use care in selecting motor for flight. Follow manufacturer recommendations. – Follow manufacturer recommendations for max lift off weight per safety code. – Attempt high-G launches only rockets having appropriate construction. | ||
6. Catastrophic motor failure | a.Temperature cycling of black powder motors | – Store motors at a consistent temperature | |
b. Improper construction | – Check all parts have been used (O-rings, ejection charge, spacers, etc.) – Check closures are tight, threads are not stripped. | ||
Rocket recovery | 7. Failure to eject recovery system | a. Motor ejects from rocket | – Use motor retainer clips or sufficient tape to provide positive friction fit of motor – Be sure that recovery system not packed too tightly – Use heat resistant adhesives in motor retention system |
b. Improper assembly of reloadable motors | – Build motor correctly following manufacturer directions – Avoid grease on delay element – Avoid crimping or damaging o-rings -Verify ejection port is clean and clear – Insure ejection charges are loaded | ||
c. Electronics failure | – Verify system integrity before first flight or after major changes – Use motor ejection for redundancy | ||
d. Failure of electronic recovery system to fire ejection charge | – Verify charge integrity with multi-tester or self-testing recovery system – Check mach lock-out settings on altimeter – Insure all hardware and electrical leads are installed properly and secured against flight loads. | ||
e. Construction/ Preparation | – Too much wadding/packed too tightly – parachute packed too tightly – obstructions within body tube | ||
TASK/STEP | HAZARD | CAUSE | PREVENTATIVE MEASURE |
8. Failure of chute to open | a. Recovery device stuck in rocket body | 1- Too much wadding 2- Recovery device too large or not packed properly 3- Insufficient ejection charge for size of body tube – see chart | |
b. Parachute burned by ejection gasses | – Use flame-resistant recovery wadding or other protection system | ||
c. Parachute shroud lines fouled | – Fold parachute carefully as described by manufacturer | ||
9. Strip of recovery system at deployment | a. Deployment occurred too early or too late | – Follow anufacturer¹s recommended maximum lift-off weight and/or computer simulation data. – Use electronic apogee detecting deployment system. – Use rocket flight simulation program to simulate flight determine best delay time. – Select shorter delays when winds are higher. The rocket will weather vane into the wind and shorter delays are required for proper recovery system activation. | |
b. Improper construction | – Use proper hardware | ||
10. Separation of recovery or other system. | a. Recovery system improperly secured during preflight prep. | – For initial flight, or subsequent flights after repair, double check that the recovery system is properly attached to the rocket/payload section/nose cone. Inspect quick links, eyebolts, or other hardware to ensure that links are closed/locked and that other hardware is intact and secured. – Insure eye bolt connector will not un-screw during descent | |
b. Failure due to wear and tear of flight operations | – Periodically inspect all components of the recovery system. Replace/repair burned or worn shock cords. Replace/repair parachutes with worn or frayed shroud lines. | ||
11. Rocket drifts into buildings / houses / trees | a. Parachute too large | Refer to parachute sizing guide and drift charts on back of checklist | |
b. Too windy | Insure winds are within limits. Consider winds aloft information | ||
c. Main parachute deploys early | -Use shear pins to secure main parachute compartment. -Use extra long shock cord and “metered deployment” of cord in drogue section. -Use proper amount of black powder in drogue ejection charge | ||
12. Rocket impacts prep area causing personal injury | Spectators not paying attention to rocket flight | – Use electronic PA system for all high power launches. – Launch Control Officer responsible for calling “Heads Up” -LCO give periodic detailed briefing to spectators on the meaning of ‘heads up’ and the corrective action to be taken -If possible, angle all flights away from spectators | |
13. Rocket impacts Buildings/houses in ballistic flight | Multiple failures | -Follow wind/altitude restrictions – see “failure to eject recovery system” |
NOTE: Preventative measure is not all inclusive and additional precautions may be required in order to maximize safe flying condition.