Dinitrogen tetroxide
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| Dinitrogen tetroxide | |
| IUPAC name Dinitrogen tetroxide | |
| General | |
|---|---|
| Chemical formula | N2O4 |
| Molecular weight | 92.011 amu |
| Appearance | Yellow-brown liquid; vapor is reddish-brown |
| CAS number | 10544-72-6 |
| MSDS link | N2O4_MSDS_pdf (http://www.airliquide.com/safety/msds/en/090_AL_EN.pdf) |
| Physical properties | |
| Density and phase at STP | 1.45 g/cm3 (?) |
| Solubility | reacts with water |
| Specific gravity | 1.44 (liquid at 20°C) |
| Crystal structure | ? |
| pH (10% solution with water) (pKa) | ? |
| Acidity constant (pKa) | ? |
| Thermal decomposition | ? K (? °C) |
| Phase behavior | |
| Melting point | 261.928 K (-11.2 °C) |
| Boiling point | 310.15 K (21.1 °C) |
| Triple point | ? K (? °C) ? bar |
| Critical point | ? K (? °C) ? bar |
| Heat of fusion (ΔfusH) | ? kJ/mol |
| Entropy of fusion (ΔfusS) | ? J/mol·K |
| Heat of vaporization (ΔvapH) | ? kJ/mol |
| Safety | |
| Ingestion | ? |
| Inhalation | Corrosive & toxic |
| Skin | Corrosive |
| Eyes | Corrosive |
| Flash point | ? °C |
| Autoignition temperature | n/a °C |
| Explosive limits | ? - ?% |
| OSHA Permissible Exposure Limit (PEL) | 5 ppm |
| NIOSH Immediate Danger to Life and Health (IDLH) | 20 ppm |
| Precautions | |
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| Solid properties | |
| Standard enthalpy change of formation (ΔfH0solid) | ? kJ/mol |
| Standard molar entropy (S0solid) | ? J/mol·K |
| Heat capacity (Cp) | ? J/mol·K |
| Density | ? g/cm3 |
| Liquid properties | |
| ΔfH0liquid | ? kJ/mol |
| S0liquid | ? J/mol·K |
| Cp | ? J/mol·K |
| Density | ? g/cm3 |
| Gas properties | |
| ΔfH0gas | ? kJ/mol |
| S0gas | ? J/mol·K |
| Cp | ? J/mol·K |
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Except where noted, all data was produced under conditions of standard temperature and pressure. | |
Nitrogen tetroxide (or Dinitrogen tetroxide) (N2O4) is a hypergolic propellant often used in combination with a hydrazine-based rocket fuel. The combination was used to fuel the Titan rockets used in the Gemini missions, and is still used today in the second stage engines of Delta II rockets. By the late 1950s it became the storable oxidizer of choice for rockets in both the USA and USSR. [1] (http://www.friends-partners.org/partners/mwade/props/rocindex.htm)
Nitrogen dioxide is made by the catalytic oxidation of ammonia: steam is used as a diluent to reduce the combustion temperature. Most of the water is condensed out, and the gases are further cooled; the nitric oxide which was produced is oxidised to nitrogen dioxide, and the remainder of the water is removed as nitric acid. The gas is essentially pure nitrogen tetroxide, which is condensed in a brine-cooled liquefier.
Nitrogen tetroxide is a brownish yellow liquid which is easily vaporized. It is a powerful oxidizer, and is highly toxic and corrosive. However, it is not affected by mechanical shock and does not react with air. Nitrogen tetroxide is always in equilibrium with nitrogen dioxide (NO2) and some nitrogen dioxide will be present in any quantity of nitrogen tetroxide (higher temperatures push the equilibrium towards nitrogen dioxide).
Nitrogen tetroxide is sometimes a component of smog.
External link
- NIOSH Pocket Guide to Chemical Hazards (http://www.cdc.gov/niosh/npg/npgd0454.html): Nitrogen tetroxide
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fr:Peroxyde d'azote
ja:四酸化二窒素