H2O2 - O2 characteristics?

Does anyone use an engine burning H2O2 with O2? Just wondered what those
characteristics might be.

Thanks,


Matt Bille
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OPINIONS IN ALL POSTS ARE SOLELY THOSE OF THE AUTHOR

In article ,
MattWriter wrote:
One of my best typos. I meant with RP-1. And I was referring to use for
launch, not for in-space thrusters only.

There are no peroxide/kerosene systems currently in operational use,
although it has been done in the past and there are several proposals for
new systems using that combination. It scores very well on handling ease
and safety, and on propellant density, but not so well on Isp.
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MOST launched 1015 EDT 30 June, separated 1046, | Henry Spencer
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