Rocket recovery system failure modes
A compilation of reasons why your rocket may no longer be in one piece
- The chute shroud lines being the same length as the shock cord, therefore the shock cord could go tight without ensuring the chute was completely out of the bay.
- Poor shock cord attachment at motor end or nose end.
- Poor Nomex placement results in burnt chute/shock cord
- Chute tangles are reduced with use of a swivel.
- Shock cords about 5m to reduce shock loads.
- Place chute so that nose and tail sections don't bash each other on decent.
- Ensure chute compartment is sufficiently sealed so that it can pressurise, primarily between the altimeter bay which should be well vented.
- Motor retention inadequate, resulting in motor being ejected rather than chute.
- Flight computer must signal continuity on pad.
- Flight computer can signal continuity but have damaged capacitor so not fire, ground test firing circuit if possible.
- Use redundant systems, two flight computers.
- Don't use smokeless powder, it is too pressure sensitive. Blackpowder substitutes behave differently and should be avoided
- Make sure e-matches are well clamped in screw terminals.
- Use acceleration tolerant switches, key switches are good.
- Align switches perpendicular to axis to avoid acceleration effects.
- Shock cord not strong enough, assume 20g loads (probably excessive)
- Use kevlar cord (heat resistant) next to ejection charge and nylon cord or tape to reduce shock load.
- Use good knots, bowlines, barrel knots and fig 8 for cord, tape knots and overhands for tape.
- Use tape to pad kevlar cord where it leaves body tube to avoid tube damage "zipper effect"
- Ground test every deployment three times, to check for repeatability
- Ejection charges are best mounted centrally on bulkheads, use eyenuts on the end of studding if required.
- Only use masking tape to adjust fits, other tape generally binds worse.
- Check friction in joints, it can change.
- Use a rape alarm so you can find the debris
- Compartments vented so that reduced ambient pressure doesn't cause premature separation.
- Vent altimeter bays symmetrically to avoid false readings from wind.
- Ensure ejection charge not going to change due to acceleration (ie use wadding).
- Use nylon shear pins (M2) to stop main deploying at drogue deployment.
- A shear pin can be used to stop the drag on the fins at motor burn out causing separation, has this ever happened?