"I'm still in favor of having a mechanical (or solid-state) switch that opens up a HPR motor ignition circuit that's independent from everything else, so that you can turn on everything else at the pad and confirm from your beeping altimeter that all the deployment charges are ready to go before you enable that airstart ignitor."
YES!!!
Totally agree... you really need something that disconnects and shunts the pyro's.
Especially when dealing with HEI motors....that are built and installed in advance.
I wouldn't think of doing anything else....
Feel free to read and contribute to this thread on airstart safety for a good discussion on this if you haven't already seen it.
The Raven doesn't have a problem with that.Now just wish today's altimeters would really support motor ignition....
Some don't arm if you have a disconnected pyro....you can't delay arming the motor till the last checklist item.
Some continue to do their continuity ping into motor ignition circuits.
The raven has 266 kOhms in series with the continuity check. Only 10s of micro-amps go through the ignitor, putting less than 1 in 100,000 the power needed to fire it.
With 4 outputs, you can do stage separation, motor ignition, apogee, and main deployments all in one, and use a separate altimeter with its own power supply for a true redundancy on the deployments. If you don't have space for full redundancy, you can off-load the staging charge to the booster's Raven and then you have a freed up output for a backup apogee or main. That's how I set up my high-altitude staged flights, with a medium-altitude deployment in case the altitude keeps my apogee charge from working.Most don't have enough channels to light motors and still handle deployments....man I'd love to have 5 or 6 channels so we can do an air-start or two and still do dual-deploy with backup chrages off of a single altimeter.... (hint Adrian...can we have an Albatross???)
For the Raven (and the RavenPlus), adding another output channel or two would bust the design on multiple fronts, including pin count, A/D inputs, and program memory.
Things get really interesting when you use "ignition controllers" to light the motors on command from the altimeter. These can fire on WAY less current than an igniter and can be incompatible with the continuity checks.
Why use "ignition controllers" you ask....because many altimeters can't fire multiple pyro's at the same time for clustered airstarts and/or there is a need to span the drogue bay with thin, breakable wires that won't support the current needed to light multiple motors... So we put a small "amplifier" at the head of the motor(s) that provides the current (from a local battery) when signalled from the altimeter.
I like to use simple pull-apart connectors to span across separating parts of the rocket. And you'd be surprised how much current tiny wires can handle if you're not worried about temperature rise.