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In Topic: Hybrid Rockets
21 January 2007 - 12:50 AM
In Topic: NH4NO3 in rockets?
09 January 2007 - 06:38 PM
In Topic: Hybrid Rockets
04 January 2007 - 06:18 AM
That made me chuckle.
Maybe he's right.... lol
In Topic: Hybrid Rockets
02 January 2007 - 09:45 PM
Actually, Liquid Oxygen is Cryogenic so yes, that would be a bit more difficult to construct, however, N2O, Beutane, and Propane are simply compressed. For this all you need is an adjustible regulator between the injector and the fuel/oxidizer tank. Which can be found fairly easily at a hardware store. I'll look into that book though, and I'm going to be e-mailing Richard Nakka and John Wickman. The book will most likely help alot, thanks man.Your questions will be answered by the book "rocket propulsion elements" wich I Use and even Richard nakka does.
I am not interested in high power rocket motors very much, so I didnt think of those techniques. I only use BP or KNO3/sugar propellant.
Probably it would be the best to ask Richard Nakka. He uses KNO3/suchrose and similar fuels but he has a unbelieveable knowledge...
One word from a mechanical engineer (me):
Do you really know how difficult the needed equipment is? Its really not easy to inject liquid oxygen into a chamber in a good regulated way.
I think I am a good engineer but I would not know how to manage the many problems you will have.
MfG
newtoolsmith
In Topic: Couple of rocket questions
06 October 2006 - 03:14 PM
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