jrkennedy2
Well-Known Member
Well, my June 1st didn't go so well. I was at a launch attempting to fly a 4 Mania on a CTI Pro75 7521M840-P, moonburner. Simed out to about 20,000'. Morning started windy but settled down just about when the window opened (1400 hours). Dual deployment computers came online fine. GPS got lock fine. Mobius camera was rolling. Igniter installed and aft closure re-tightened. Countdown 5,4,3,2,1, launch... At about .25 seconds after initial ignition, BANG! The motor seems to have blocked the exhaust nozzle and over-pressured. It blew the rear motor case ring out, nearly cutting a coin out of the exhaust deflector (pretty cool to see, actually). The Aero Pac retainer split cleanly at the pressure area (rim). The recoil of the case letting go shot the 6gr case through the top of the rocket, rendering to dust the: 2 RRC2s (the entire av-bay), 1 Eggfinder GPS, and 1 mobius camera as well as mauling the harnesses badly. I was unable to locate the rear case ring and nozzle. They probably bounced to the next county. I found 5 of the grains in pretty good shape and the sixth one fractured and in pieces with some bits burned-up. Each grain showed tearing of the paper casing indicating that at least some resistance was felt to the grain movement. I utilized Gorilla Glue to fix the grains in the liner. I used a dowel to ensure the alignment of the off-center bores were straight. I verified the igniter was all the way to the top by measuring the length on the cardboard tube (included) against the length of the 6 grains. Check, check, check...
My only guess is the bottom (closest to the nozzle) grain (G6 for now) came loose as the pressure started to rise and subsequently blocked the nozzle causing over-pressure. During assembly, there was a small space, about 1, between the G6 and the throat of the nozzle, preserved by the liner. By this I mean the liner met the nozzle and kept that space from G6. I assume that space is the combustion stabilization area since the bores are offset and need a little room to get the gasses moving a bit better toward the nozzle. Also, it would have been VERY hard to get the igniter dowel (or cardboard tube) to make any steeper a turn without that space. Any thoughts what went wrong (what I did wrong)? I have some picts to help illustrate.
I pretty sure it was assembler's error (me) not CTI.

My only guess is the bottom (closest to the nozzle) grain (G6 for now) came loose as the pressure started to rise and subsequently blocked the nozzle causing over-pressure. During assembly, there was a small space, about 1, between the G6 and the throat of the nozzle, preserved by the liner. By this I mean the liner met the nozzle and kept that space from G6. I assume that space is the combustion stabilization area since the bores are offset and need a little room to get the gasses moving a bit better toward the nozzle. Also, it would have been VERY hard to get the igniter dowel (or cardboard tube) to make any steeper a turn without that space. Any thoughts what went wrong (what I did wrong)? I have some picts to help illustrate.
I pretty sure it was assembler's error (me) not CTI.





