marcusSRG
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Ok, I made a post a while back regarding various electronics switches and shunts. That was a good thread, but the discussion went more towards switches and phono jacks. I'm still hung on shunts a little but I think I got it...I just want to get a couple of things cleared up.
I know a shunt is basically a safety switch along the connection between a timer/accelerometer channel output and the rocket's airstart/staging igniter(s). This switch can be opened or closed, depending on setup, to safe the igniter(s) from an accidental output from the electronics...
BUT, doesn't a shunt still allow continuity of the outboards to be verified by the electronics WHILE it's engaged?? I attached a crude schematic of two possible "igniter safing" setups...you'll see I'm no electrical engineer!
![SHUNT2.jpg SHUNT2.jpg](https://cdn.imagearchive.com/rocketryforum/data/attachments/96/96139-0e18e66014917e79900e941962b0beab.jpg)
So...isn't picture "A" a true shunt? Here the shunt would be "engaged" when the switch is closed....and the electronics should be able to verify continuity, right?? In picture "B", the switch would inhibit a continuity check for sure...but would a good TRA RSO consider "B" to be a proper shunt??
I plan to apply all of this stuff to my LOC Ultimate and 429-SS rebuilds for airstart flights. I will be using a PET2 timer. To conform with TRA code I'll be safing my outboard igniters with shunts (as advised here) as well as utilizing the PET2's pull-pin AND g-switch arming feature to lock out the timer until the rocket is prepped, as demonstrated by dixontj93060 with his two stager here: https://www.rocketryforum.com/showthread.php?21235-Two-Stager
Thanks.
I know a shunt is basically a safety switch along the connection between a timer/accelerometer channel output and the rocket's airstart/staging igniter(s). This switch can be opened or closed, depending on setup, to safe the igniter(s) from an accidental output from the electronics...
BUT, doesn't a shunt still allow continuity of the outboards to be verified by the electronics WHILE it's engaged?? I attached a crude schematic of two possible "igniter safing" setups...you'll see I'm no electrical engineer!
![SHUNT2.jpg SHUNT2.jpg](https://cdn.imagearchive.com/rocketryforum/data/attachments/96/96139-0e18e66014917e79900e941962b0beab.jpg)
So...isn't picture "A" a true shunt? Here the shunt would be "engaged" when the switch is closed....and the electronics should be able to verify continuity, right?? In picture "B", the switch would inhibit a continuity check for sure...but would a good TRA RSO consider "B" to be a proper shunt??
I plan to apply all of this stuff to my LOC Ultimate and 429-SS rebuilds for airstart flights. I will be using a PET2 timer. To conform with TRA code I'll be safing my outboard igniters with shunts (as advised here) as well as utilizing the PET2's pull-pin AND g-switch arming feature to lock out the timer until the rocket is prepped, as demonstrated by dixontj93060 with his two stager here: https://www.rocketryforum.com/showthread.php?21235-Two-Stager
Thanks.
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