Copperheads!
Actually, I would think they would use something very energetic to ensure ignition. They can't swap out the igniter if it fails!
Like rstaff3 said. Something like this:
https://www.eba-d.com/assets/produc...n-CapabilitiesSht-Web-Low-Res-For-Gen-Use.pdf
Steve Shannon
Thank you to you and Rstaff3 for the needed details, and the rest for the laughs! I had assumed (hoped?) that the military had something more elegant (and of course expensive) than an e-match, but couldn't find any specifics!
Like rstaff3 said. Something like this:
https://www.eba-d.com/assets/produc...n-CapabilitiesSht-Web-Low-Res-For-Gen-Use.pdf
Steve Shannon
I want one
unless I'm mistaken in that the O25k is a commercial HPR version of the Aim-9 motor
According to Wikipedia, the engine is a Hercules/Bermite MK36 Solid Fuel Rocket.
Does anyone know what "MK 36" means? It's listed in the name (with parenthesis around it) of the first sidewinder variant and in the name of the rocket motor.
There's also this: https://www.govconwire.com/2016/07/...-for-sidewinder-block-ii-missiles-production/
I think I'll be backing out of the conversation a little, since I'm quite confused right now.
Adapting these to HPR Head-End-Ignition (HEI), as Aerotech is pursuing, also requires some thought to safety. If you review the linked PDF, you'll see a schematic that requires two independent 'arm' inputs plus a 'fire' signal to initiate ignition. For a two-stage configuration, with HEI for the upper stage, this adds an interesting margin of safety.
https://www.e2v.com/resources/account/download/28
Two words: Zirconium and Boron.
https://en.wikipedia.org/wiki/Pyrotechnic_initiator
Three words: Don't go there.
Kurt
Help me understand Kurt. BKNO3 is used for rocket ignition, isn't it?
Help me understand Kurt. BKNO3 is used for rocket ignition, isn't it?
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