C-Stoff
This article has multiple issues. Please help improve it or discuss these issues on the talk page. (Learn how and when to remove these template messages)
|
C-Stoff (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
Messerschmitt Me 163 aircraft that employed this fuel system. Another hazard was toxicity to humans of each of the propellants.[1]
C-fuel
After the war, Allied studies into rocket propellants continued with engines such as the Armstrong Siddeley Beta, under the name "C-fuel".[2]
See also
- List of stoffs
- UDMH
References
- ISBN 3-8289-0294-4.
- ^ "United Kingdom Aerospace and Weapons Projects: Rocket Engines". Skomer. Archived from the original on 2008-04-22.