C-Stoff

C-Stoff ({{#invoke:IPA|main}}; "substance C") was a reductant used in bipropellant rocket fuels (as a fuel itself) developed by Hellmuth Walter Kommanditgesellschaft in Germany during World War II. It was developed for use with T-Stoff (a high-test peroxide) as an oxidizer, which together with C-Stoff as the fuel, forms a hypergolic mixture.

Methanol	CH3OH	~57% by weight
Hydrazine hydrate	N2H4 · H2O	~30% by weight
Water	H2O	~13% by weight
Catalyst 431	K3[Cu(CN)4]	potassium tetracyanocuprate(I)

The proportions of the components in C-Stoff were developed to catalyse the decomposition of T-Stoff, promote combustion with the oxygen released by the decomposition, and sustain uniform combustion through sufficient quantity of the highly reactive hydrazine. The combination of the C-Stoff, used as a rocket fuel, with the T-Stoff used as the oxidizer, often resulted in spontaneous explosion from their combined nature as a hypergolic fuel combination, necessitating strict hygiene in fueling operations; there were numerous catastrophic explosions of the Messerschmitt Me 163 aircraft that employed this fuel system. Another hazard was toxicity to humans of each of the propellants.<ref>Template:Cite book</ref>

C-fuel

After the war, Allied studies into rocket propellants continued with engines such as the Armstrong Siddeley Beta, under the name "C-fuel".<ref name="skomer">{{#invoke:citation/CS1|citation |CitationClass=web }}</ref>

See also

• List of stoffs
• UDMH