•  CAMERAS OVERHEATED

    • Design heat transfer-optimized aeroshells with thermal fins (heatsink)

    • Cover cameras with foil or foam or something that can stay on the launch rod and shed once the rocket launches

  • DENNIS GPS took 15 minutes to lock

    • Avionics should save and load GPS ephemeris data to speed up the time to lock. This will allow us to vastly improve the minimum time to launch after avionics power up, which is important when all your cameras overheat :(

  • Booster camera got crushed and destroyed SD card

    • Might be a good idea to remove some of the material of the plastic case around the SD card slot of the keychain camera

    • Or remove the case completely and replace it with something sturdy, e.g. aluminum shell

    • Replace “springy” SD card slots with “locked” SD card slots

    • If we switch to only split cameras (like the Runcam split 4), it might be a good idea to put the main part of the camera inside of the rocket body and just have the lens sticking out. This would provide better protection from crashes, the sun, and would reduce the need for large aeroshells. Possible downside is increased integration complexity.

  • Lost the main parachute on booster once again

    • Longer deployment delay?

    • Drogue on booster?

    • Reinforce the loop at the bottom of the parachute, and maybe do some repetitive stress tests on that

    • Buy parachute from a different supplier

    • Multiple chute deploy for redundancy?

    • Data review shows the acceleration from the booster main deployment occurred ~10 seconds after the piston fired. A possible explanation for this is the main chute did not exit the deployment bag right away. Maybe the main parachute was packed too tightly. Then for 10 seconds, the booster picked up speed and possible twisting of the lines before the parachute deployed and snapped.

  • Tender Descenders didnt fire

    • Check to make sure wires aren’t shorted

    • Double check firebolts being used are not being reused and passed all testing

    • Only use cots TDs

    • Make sure battery voltage is high enough to fire

    • Double check that right amount of black powder is used

    • Make sure black powder doesn’t get wet.

      • The space used for integration was a leaky hangar. .

    • Use armored wires/more shielded wires for e-matches to prevent shorting

  • Sustainer was fully loaded with HEI for a long time

    • make new forward closure such that it can be properly integrated with hei in later? maybe a thread in hei section

    • find high temp gasket that doesn’t take 48 hrs to dry

    • more o rings on hei so full motor pressure isn’t held by 1 o ring

    • new hei design that means we rtv put in the nozzle and liner and add the grain and igniter later without risk of cracking

  • HEI avionics integration

    • Shunt and diode cable harness worked really well, however we should’ve characterized the voltage drop better

    • The combination of the depleted sustainer battery and voltage drop across the diode meant that we launched with the telemega in the “red” state for the HEI channel. There was still plenty of power to ignite the HEI though.

    • To integrate the sustainer with the HEI, we simply wrapped the wire around the HEI bolts. A better way would be to use “ring terminals” to securely mount the cable harness to those bolts.

  • flight cameras turned off before launch

    • put hei on booster and then ignition sequence turns on all cameras (would somehow be hooked up to avionics) just before lighting the booster hei

    • Make cameras not independent (turn on with avionics)

  • Avionics turned on while driving to FAR

    • Properly secure mission package. We forgot to screw in the avtower before the day of the launch. Had we not caught this at FAR, it would have led to catastrophic failure.

    • Drive rocket to FAR without a “complete” complete integration so theres no risk of ignition

    • Redundant screw switches (an “and” gate maybe)

    • One idea is to transport the screw switches without the screws. If the switch is positioned close enough to the rocket wall, we can go to the pad with the necessary screws to turn the rocket on. This would make an accidental power-on almost impossible

    • Backup avionics battery? Future designs could possibly consider an easier hot swap of batteries, but I think we should focus on ensuring batteries are charged prior to launch and double ensure that nothing turns on before we want it to. Current avionics power architecture supports “on-the-pad charging” should we need to top up the batteries.

  • Booster bolts scratched inside of fin can

    • properly countersink bolts including going into nozzle carrier so they don’t poke out at all

    • Switch to 82 degree countersink bolts that are more common and can be used with torx heads

      • Match drill and match countersink carriers and case for guaranteed flat finish

    • Put bolts through fin can maybe?

  • Booster nozzle carrier bolts were sized incorrectly

    • actually use the ones linked in solidworks

    • drill holes a little deeper in nozzle carrier

    • use the correct countersink 

    • Could cut a relief on the bolt head to allow them to pull closer

  • Stripped bolt heads

    • switch to torx 

    • get folding key sets so we don’t spend forever trying to find the one key that works

    • Do accurate bolt calculations

      • T =  K*d*F

      • K = nut factor (usually .2, lower with lubrication)

      • d = bolt major diameter

      • F =  axial force on bolt needed (F = P*0.75*(pi*(D/2)^2))

      • Thread engagement must be at least 1.5x the bolt diameter

  • Sustainer transition melted

    • Use a more heat resistant material

  • Tube sanding (fin can, motor case, nozzle components, FRR, FC, etc.)

    • Sanding tubes is a pain in the ass and doesnt have to be

    • Find a way to machine the inside and outside of the cases (just the interference ends, doesnt need to be the whole thing)

    • Talk to todd about how to machine inside long hollow tubes

    • Buy a proper tube sander kit

    • Proper tolerancing

      • Clearance fit vs. press fit

      • Different tolerance for one end of fin can tube (the end that goes over bolts near boattail)

    • More rigorous fit checks before launch rehearsal

  • Pad cameras turned off before launch

  • Angry Goat was poorly characterized

  • Motor case bolts may have bent (haven’t dis-integrated but im guessing they did)

    • Result of pressure spike of errosive burning

    • Try to use less fynocyl in designs because it 

  • Didn’t have everything we needed for launch at FAR

    • make launch day packing list that is packed morning of and reviewed by the packing lead

    • Teams who arent integrating should help pack

  • Ignition stick too big

    • ⅛” dowel would be better (needs flex to put inside motor and not block a large portion of the nozzle throat

  • Away teams

    • Give both away teams cameras or consolidate them into one group

    • Food options for away teams in case launches get delayed

    • Livestream from Away site?

    • All avionics members using the groundstation should practice telemetry callouts. We never know exactly what to say and FAR people really care about current altitude and deployment status.

  • Radio coms/Telemetry

    • Coordinate with FAR and other people that launch in regard to their used channels (we can change the channel only if the TeleMega is not in Padmode aka vertical)

    • Practice Radio coms during launch rehearsals, and how to switch channels

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