Quoted
Originally posted by Hood
I've a BIS study paper on British HTP rockets for some info. I'll work on the details.
What I love is the simplicity, there are no boilers or burners or combustion chambers. HTP rockets were also quite basic. I'm thinking along the lines of a basic tapered tube, HTP goes in, decomposes over catalyst, steam at 500-600c then goes into smaller end and compresses into a turbine, then another to make full use of the steam which then goes out via a rear-facing jet-type exhaust, some tapped off from heating and de-icing. Turbine 1 drives the propeller, and Turbine 2 drives cabin pressurisation system and a cruise turbine for the propeller. Looking at 4-5000shp from it. If it can't be done at 600c then its time to add some kerosene... and all the high-tempurature metallurgy problems that brings.
HTP is tricky stuff but I think it can be tamed.
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