Andrew wrote:

AC> Interesting that the major hazard to people on the ground appears to be 
AC> OMS propellants. Yet another data point in favor of non-toxics.

By sifting through my papers, I came across a copy of a Final Report
of 1985 "Ignition Characterization Of LOX/Hydrocarbon Propellants"
Contract NAS 9-16639 from Aerojet TechSystems Company.
The work was done to eventually replace toxic NTO/MMH in small
thrusters.
One of the propellant combinations they studied in more detail was
GOX/Ethanol LOX/Ethanol. Besides igniters and small test engines
there was the intention to build a LOX/HC truster to fit in the
envelope of the Shuttle RCS engine. As arguments to abandon NTO/MMH
not only the toxicity but also the much lower handling costs of LOX/HC
are mentioned. Unfortunately the pictures in the paper are of
poor quality as my copy was taken from a microfilm I lent from
a library.

Hans


Hans Ulrich Ammann
mailto:[EMAIL PROTECTED]
http://www.spl.ch

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