Instead of running a purge you can keep the fuel flowing through the igniter to keep it cool. Thomas On Mon, Oct 28, 2013 at 10:59 AM, Lloyd Droppers < lloyd.droppers@xxxxxxxxxxxx> wrote: > Ben's got the answer there, but if your running a test stand two additions > are > > -you need to think though the flow rate after main chamber ignition, i.e > you will be probably be running the igniter for a second or two after main > chamber ignition, so make sure you don't shift into some really hot O/F. > If you are on a test stand it is easier to make sure your igniter feed > pressures are 50% over PC or greater and you should be fine, on a vehicle > you don't always have that luxury. > > -Also, if you can, running a purge through the igniter after main chamber > ignition at about the pressure as PC will save the igniter from torching in > the case of leaks and some instability. Probably not worth it on a > vehicle, but for injector characterization tests it is very worth it. > Unless you really enjoy rebuilding igniters i guess. > > Lloyd > > > On Sat, Oct 26, 2013 at 5:22 PM, Ben Brockert <wikkit@xxxxxxxxx> wrote: > >> 1. Doesn't matter. Igniters are often run heat sink mode, and heating >> goes up with higher pressures, so running at low pressures is >> advantageous for minimizing heating. At the same time you do want to >> run choked so that you can detect go/no go with a pressure transducer. >> That sets the reasonable minimum around 30psi, so for off-nominal >> propellant conditions a nominal operating pressure of 60-100 psi is >> good. If tank pressure is lower than that then you take what you can >> get. >> >> 2. If the igniter is plumed to main feed pressure, by nature you can't >> get chamber pressure to flow up the igniter lines because there has to >> be pressure drop across the rocket injector for the rocket to rocket. >> You can add check valves if you're really worried about it, but I've >> never bothered. If you hard start the engine or have severe >> instability the Pc can be higher than propellant pressure, but then >> you have other problems worse than igniter trouble. >> >> A much more realistic concern is making sure that all of the >> connections on the igniter are absolutely leak-free. Leaks will turn >> into (likely rapidly enlarging) hot gas leaks when the igniter is off >> and the engine is on. >> >> It's common to have 1/8" tubing feeding small igniters. Use stainless >> tubing, the weight difference with aluminum is inconsequential. Never >> use aluminum tubing smaller than 1/4", it can't survive even small >> fires when pressurized. >> >> Ben >> >> On Sat, Oct 26, 2013 at 5:57 PM, Graham Sortino <gnsortino@xxxxxxxxx> >> wrote: >> > Apologies, in advance as I'm almost positive this question was already >> > answered but I can't seem to find the responses. >> > >> > Re-phrased: >> > >> > 1. When designing a (GOX/Ethanol) igniter should the chamber pressure be >> > higher or lower then the main engine pressure? Also, are there any >> rules for >> > choosing an injector pressure relative to the main engine pressure? >> > 2. If the igniter pressure should be lower than the chamber pressure >> then >> > how does one prevent propellants flowing back through the injector >> orifices? >> > >> > Thank you very much. >> > Graham >> > >> > On Thursday, May 19, 2011 10:16 AM, Joel Scotkin >> > <arocket@xxxxxxxxxxxxxxxxxxxx> wrote: >> > On 05/18/2011 10:45 PM, Robert Watzlavick wrote: >> >> I'm going to be working on an augmented spark igniter (ASI) to try and >> >> improve the starting of my 250 lb LOX/kerosene motor. I was wondering >> >> about the chamber pressure for the igniter - I would think it needs to >> >> be >= than the main chamber pressure to keep it from flowing back into >> >> the igniter. Am I missing something? I've noticed that some designs >> >> shut the igniter off after a few seconds and in that case, how do you >> >> keep from the gases from the main chamber from backing up through the >> >> igniter orifices and into the feed lines? The few igniter pictures >> >> I've seen show small solenoid valves that typically aren't rated for >> >> enough pressure to handle the main propellant tank pressures. My >> >> kerosene tank pressure is ~490 psi (large drop through cooling jacket) >> >> and the LOX tank pressure is ~340 psi. >> >> >> > >> >> Thanks in advance, >> >> -Bob >> >> _______________________________________________ >> >> aRocket@xxxxxxxxxxxxxx >> >> http://exrocketry.net/mailman/listinfo/arocket >> > >> > _______________________________________________ >> > aRocket@xxxxxxxxxxxxxx >> > http://exrocketry.net/mailman/listinfo/arocket >> > >> > >> >> >