David Weinshenker wrote:

Henrik Schultz wrote:

Hiya All,

I intend to make some experiments with 85% H2O2, and a kerosene derivate
(most probably JP-4). I am however confused as to the best way to burn this
mix, as it seems as there are different routes one can take.

Method 1) One source (isn't it the ERPS site?) mentions something along the
line of "Catalytically decompose the H2O2 and then inject kerosene in the
hot gas stream, which essentially doubles the Isp." This is simple, in the
sense that it alleviates the need for an igniter. However, conceptually it
doesn't match any methods I've seen described in Sutton or Huzel/Huang
(perhaps except for the gas/liquid jet injectors).

Method 2) Another source works with traditional injection and impinging the
propellants into the combustion chamber, which seems to work under the
assumption that heat is already present in the chamber to get the reaction
going (igniter). I have a strong preference for this, as it allows us to use
stabilized H2O2.

Here are my questions:

Has anyone of you ever tried method 2) ?

Am I right in assuming that method 2) is self-sustaining, given a properly
sized combustion chamber, i.e. will the H2O2 at 85% produce enough heat to
both vaporize the water content as well as ignite the kerosene?

Thanks for any input you can provide!


Hmmm... ERPS' actual testing so far has only been with monopropellant
engines... however, in "Ignition!", John Clark writes of Navy work in
the 1950's with peroxide/kerosene - he notes that method 1 (precatalyze
the H2O2) was the safest and most reliable, and that it was a problem
to get clean ignition and smooth combustion with a "direct ignition"
engine (method 2).

The British, in the "Gamma" engines used in the Black Knight/Black Arrow rocket projects, also used a pre-catalyzed H2O2 stream with the fuel injected downstream of the catalyst.

-dave w

As long as you have a reasonably studly igniter running in the main chamber (for oneshot use an Estes D6-0 motor works quite well), treating them like any other non-hypergolic propellants should work. Your mileage may vary, don't try this at home, warranty void if seal broken...


--
Doug Jones, Rocket Engineer
XCOR Aerospace
POB 1163
Mojave CA 93502
(661) 824-4714

_______________________________________________
ERPS-list mailing list
[EMAIL PROTECTED]
http://lists.erps.org/mailman/listinfo/erps-list

Reply via email to