|Preferred IUPAC name
3D model (Jmol)
|Molar mass||114.15 g·mol−1|
|Melting point||−68.9 °C (−92.0 °F; 204.2 K)|
|Boiling point||135 °C (275 °F; 408 K)|
Std enthalpy of
|Flash point||29.4 °C (84.9 °F; 302.5 K)|
Except where otherwise noted, data are given for materials in their standard state (at 25 °C [77 °F], 100 kPa).
|what is ?)(|
2-Dimethylaminoethylazide (DMAZ) is a liquid fuel being investigated for use as a spacecraft propellent to replace the toxic, carcinogenic monomethylhydrazine. It is a member of the competitive impulse non-carcinogenic hypergol (CINCH) family which were assessed as a replacement for hydrazine-derived propellants.
- Mellor, B. (2004). "A Preliminary Technical Review of DMAZ: A Low-Toxicity Hypergolic Fuel". Proceedings of the 2nd International Conference on Green Propellants for Space Propulsion: 22. Bibcode:2004ESASP.557E..22M.
- "Army Develops New Fuel". Spacedaily.com. February 23, 2000. Retrieved July 12, 2014.
- Michael J. McQuaid (April 2004). "The Structure of Secondary 2-Azidoethanamines: A Hypergolic Fuel vs. a Nonhypergolic Fuel" (PDF). ARL-TR-3176. Army Research Laboratory.
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