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Funny,
Peter from Danmark and myself were amateur
rocketeers.
Rocket engines burn more stable under pressure. Typical
combustion chamber pressure is 75 Bar.
So its possible but complex. I just installed on my
sub 2 seperate air systems.. might be better.
Groet Emile
today is rocket day and will
be luanching a 15 lb v2 copy expect to reach an altitude of 6000 ft. i know
this is off subject but i remember the sub that used rocket motors for a gas
generator for the emergency ballast. i was wondering if anyone did pressure
study on rocket motors to see if they were stable under pressure. my thought
is that they are self oxidizing and desinged around an internal pressure of
about 200 lbs. while external pressure should not mater in the combustion, i
have seen enough of these thing go boom that i would like to see some testing
before using. the report from the guy that used this system from a shallow
depth was that it was deafening.
rick m
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