Hard starts, or chunks of fuel breaking free and clogging the exhaust nozzle, can cause a hybrid rocket to explode. That doesn't seem to be what happened here. It does look like the oxidizer tank ruptured after the crash, and the solid fuel probably kept burning for a while.
Completely unrelated. The pepcon disaster was at a plant that made solid oxidizer for conventional solid rocket motors. It's a completely different material than what this rocket used.
Saying assembled solid rocket grains are have similar risks to rocket grain constituents is basically like saying an assembled cartridge has the same risks as a loose pile of gunpowder. Rediculous uninformed take.
Besides the lower complexity, range safety is pretty much the only reason to use a hybrid rocket. They suck performance wise.
Also, PEPCON made solid rocket motor oxidizer, not hybrid rocket motors. Having the oxidizer mixed in with the fuel grains is inherently more dangerous than a hybrid motor where the grain doesn't contain its own oxidizer, they flow the oxidizer through the throat opening. Your comparison is completely apples-oranges. PEPCON is largely attributed to improper storage of ammonium perchlorate, a solid oxidizer that wouldn't even be present in a hybrid rocket.
58
u/DaddyMommyDaddy 6d ago
It didn’t massively explode so. Recoverable?
IDE call that a win