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There are some in the Space Shuttle Systems Handbook, Vol II (JSC 11174) - Section 11. Here's an excerpt.


I'm going to say yes, depending on how loose you want to be with definitions. Hydrogen peroxide as rocket fuel is decomposed by passing it through a metal catalyst screen, producing water, oxygen, and heat. At 90% concentration the temperature is around 800C (see figure 2). The autoignition temperature for kerosene is 210C. It worked for the Bristol Siddeley ...


Supposedly Rocket Lab is using such a fuel for their kick stage using the Curie rocket engine. Likely it is using their proprietary Viscus Liquid Mono-propellant.


It depends what you mean by green. All rockets end up producing vast quantities of greenhouse gases of a variety of types and degrees of harmfulness to the environment (even water vapor is a greenhouse gas). But apart from greenhouse gas emissions many fuels are also dangerous chemicals in their own right that leave toxic residues or pose leak risks or have ...


TL;DR: The result will probably be mostly water with significant proportions of carbon dioxide and nitrogen gas. Small proportions of copper(II) oxide and hydrochloric acid may also be released. There could be other species like nitrogen oxides, chorine oxides, unburnt CuCl2, and other carbon compounds that I'm not considering. I'm not an expert on ...

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