>> I read alot about nitrous oxide as the oxidizer in a hybrid but what
>> about plain oxygen (not LOX)?
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>force it into the combustion chamber. And if you use LOX you need
>pumps.
I have not flown a hybrid motor, but I think liquid N2O is actually
delivered to the combustion chamber and vaporized at the injector.
LOX can be pressure fed, without pumps, although you will need a
pressurization system probably using nitrogen or helium.
The only problem with N2O is that you have to get it very hot before
it "works", so motor ignition is more difficult.
Alan
Alex Mericas - 30 Sep 2004 17:27 GMT
It may be liquid at the injector, but I think if vaporizes
instantly. And N2O is self-pressurizing.
Getting it hot enough to oxidize is not a problem in practice. I
personally like the non-pyro method where you fill the combustion
chamber with GOX and then light a strip of steel wool
electronically. The pyrotechnic method, using a chunk of APCP,
works nicely too. WestCoast uses BP with an wetting agent to do the
same.
>>> I read alot about nitrous oxide as the oxidizer in a hybrid but what
>>> about plain oxygen (not LOX)?
[quoted text clipped - 17 lines]
>
> Alan
Rusty - 30 Sep 2004 17:52 GMT
> It may be liquid at the injector, but I think if vaporizes instantly.
> And N2O is self-pressurizing.
[quoted text clipped - 25 lines]
>>
>> Alan
Where can i find plans on the injector portion of the motor, this seems
to be the tricky part