Hi Bruce

Here's a link with info about hydrazine.

Ken

http://www.asi.org/adb/04/03/09/hydrazine-info.html

...Chemical Properties

Hydrazine is a powerful reducing agent. It is
attractive as a reducing agent due to its high
hydrogen content, and friendly by-product of nitrogen.
It will reduce a number of important metal salts to
the element, including silver and nickel.

Producing 148.6 kcal/mol in its oxidation reaction,
hydrazine has an impressive affininty for oxygen:

N2H4 + O2 = N2 + 2 H2O

It is used in this capacity to remove oxygen from
boiler systems, and as an additive to many substances
to prevent oxidative deterioration...


--- Bruce Crowder <[EMAIL PROTECTED]> wrote:
> 
> 
> Hi Ken,
> 
> Any idea what the energy content is of a kg of
> hydrazine would be?
> 
> -Bruce
> 
> 
> *~*~*~*~*~*~*~*~*
> 
> 
> Date: Tue, 10 Feb 2004 02:28:28 -0800 (PST) 
>    From: Ken Gotberg <[EMAIL PROTECTED]> 
> Subject: Re: Solar to Noncarbon Fuels Other Than H2 
> 
> Hi Murdoch, Greg, and April 
> 
> Hydrazine is a liquid at normal temps (mp 2C, bp
> 113C) 
> and while no longer used as a rocket booster fuel,
> it 
> is used for positioning/microcontroller jets.  The 
> technology is fairly developed now and could make 
> sense as an earthbound vehicle fuel.  Nitrogen 
> compounds are used in explosives due to high 
> energy/power densities and I’m not sure how big a 
> potential problem this is, perhaps on the same order
> 
> as H2 without the storage problems.  People
> developing 
> rockets face the same problems as, more so, trying
> to 
> get the most useful energy out of a fuel with the 
> least amount of mass.  Noncarbon fuel alternatives
> at 
> this juncture are in electric storage (batteries, 
> ultracapacitors,?), mechanical storage in things
> like 
> flywheels, and various fuel cells.  Probably others 
> that list members may know about. 
> 
> One more possibility to look at and N2 is available 
> everywhere, ~800,000 ppm in the atmosphere versus
> ~350 
> ppm for CO2 used in biofuels.  There are other 
> nitrogen fuels besides hydrazine that may also be 
> potential candidates.  Here’s a link to rocket fuels
> 
> 
> 
> And about hydrazine 
> 
> http://www.astronautix.com/props/hydazine.htm 
> 
> Fuel: Hydrazine. Fuel Density: 1.01 g/cc. Fuel 
> Freezing Point: 2.00 deg C. Fuel Boiling Point:
> 113.00 
> deg C. 
> 
> Hydrazine (N2H4) found early use as a fuel, but it
> was 
> quickly replaced by UDMH. It is still used as a 
> monopropellant for satellite station-keeping motors.
> 
> Hydrazine marketed for rocket propellant contains a 
> minimum of 97 per cent N2H4, the other constituent 
> being primarily water. Hydrazine is a clear, 
> water-white, hygroscopic liquid. The solid is white.
> 
> Hydrazine a toxic, flammable caustic liquid and a 
> strong reducing agent. Its odour is similar that of 
> ammonia, though less strong. It is slightly soluble
> in 
> ammonia and methyl-amine. It is soluble in water, 
> methanol, ethanol, UDMH, and ethylenediamine. 
> Hydrazine is manufactured by the Raschig process, 
> which involves the oxidation of ammonia to
> chloramine, 
> either indirectly with aqueous sodium hypochlorite
> or 
> directly with chlorine, and subsequent reaction of 
> chloramine with excess ammonia. Raw materials
> include 
> caustic, ammonia, and chlorine; these are 
> high-tonnage, heavy chemicals. The cost of anhydrous
> 
> hydrazine in drum quantities in 1959 was $ 7.00 per 
> kg. The projected price, based on large-scale 
> commercial production, was expected to be $ 1.00 per
> 
> kg. Due to environmental regulations, by 1990 NASA
> was 
> paying $ 17.00 per kg. 
> 
> Best regards, 
> 
> Ken 
> 
> 
> 
> 


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