Malfunctioning Engine Statistical Survey
M.E.S.S.

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Manufacturer
AeroTech
Designation
J825R-M
Type
reload
Date code
7021501
Failure date
Oct 29, 2016
Location
Prairie Hill, Tx
Temperature
88 ℉
Ejection end blown out
Casing split
Burning propellant ejected
Comments
The motor was assembled per the included instructions 2 days prior to the flight. No issues were noted during assembly. The case ruptured just below the forward closure, with the forward closure and seal disk being blown clear from the rocket. These were not recovered. The liner and grains were ejected from the case. They were not burning at the time they were ejected, but did re-ignite while in the air. The failure happened shortly after ignition. Approximate burn time was 0.25 seconds.
Status
accepted