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TheChemist

Member Since 17 Oct 2006
Offline Last Active Nov 24 2006 08:26 PM
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Posts I've Made

In Topic: lead nitrate

10 November 2006 - 01:36 PM

Used as an oxidiser, the oxidizing part of Pb3O4 ([Pb(II)O]2Pb(IV)O2) is the Pb(IV).
I guess the Pb(IV) is stabilized in this compound as compared to pure Pb(IV)O2 that is a strong oxidizer.
PbO2 will ignite fx. red phosphorus and hydrogensulfide (and most likely a lot of other substances) on contact.

In Topic: lead nitrate

10 November 2006 - 10:45 AM

I have now tried the most well known way to produce Pb3O4, that is heating PbO on an iron plate at 450C to oxidize the lead further. ( I used a spoon on a gas burner)
For some reason this did not work as it was supposed to <_<.
Maybe the burner removed all the oxygen needed for the process.
By the way, Pb3O4 is really (PbO)2PbO2, is there any particular reason for using Pb3O4 and not PbO.
When I tested it in the lab they colour the flame in the same way when burned.
I will keep looking, and return if I find anything useful.

In Topic: lead nitrate

10 November 2006 - 08:04 AM

Does anyone know how to make lead tetraoxide? I tryed to mix it up with NaOH but nothing happened. Anything i am missing?

thnx


Before I dig into all of my books, is it the Pb3O4 you are interested in? (This is red and has been used as colour in paint) or the PbO2, a powerful oxidizer that can be used in matches together with red phosphorus.

In Topic: What mix you use for sucrose+KNO3 combustible?

19 October 2006 - 05:19 PM

There are several good reasons for not using the stoichiometric mixture (given by the math) for this reaction.
First of all this mixture is considered an explosive!
Second; the main areas of (peaceful) use are:

Smoke screens:
Incomplete combustion will give more smoke.

Solid state rocket fuel:
The fuel should be easy to cast and you do not want the fuel to damage the rocket by exploding or burning with too high a temperature.

From Richard Nakka's Experimental Rocketry Web Site: http://members.aol.c...on/sucrose.html

"The 65/35 (sucrose/nitrate) ratio has proven to give the best overall performance combined with acceptable casting qualities. Theoretically, the highest specific impulse is delivered at a 66/34 ratio, although the standard 65/35 ratio tends to be used by most experimentalists. There are three reasons for this:

The propellant characterization data has been obtained mainly for the 65/35 ratio
The performance difference is slight (about 1%).
The combustion temperature rises sharply with increased O/F ratio. At the 65/35 ratio, steel nozzles suffer no erosion, as there is an adequate margin between the theoretical flame temperature (1450C) and the melting point of steel (approx. 1500C). At higher O/F ratios, this margin is reduced such that a small error in weighing during preparation could result in a heat damaged nozzle."