Dinitrogen tetroxide
Full structural formula
Full structural formula
Space-filling model
Space-filling model
Nitrogen dioxide at different temperatures
Nitrogen dioxide at −196 °C, 0 °C, 23 °C, 35 °C, and 50 °C. (NO
2) converts to the colorless dinitrogen tetroxide (N
2O
4) at low temperatures, and reverts to NO
2 at higher temperatures.
Names
IUPAC name
Dinitrogen tetroxide
Identifiers
3D model (JSmol)
ChEBI
ChemSpider
ECHA InfoCard 100.031.012
EC Number
  • 234-126-4
2249
RTECS number
  • QW9800000
UNII
UN number 1067
  • InChI=1S/N2O4/c3-1(4)2(5)6 checkY
    Key: WFPZPJSADLPSON-UHFFFAOYSA-N checkY
  • InChI=1/N2O4/c3-1(4)2(5)6
    Key: WFPZPJSADLPSON-UHFFFAOYAS
  • [O-][N+](=O)[N+]([O-])=O
Properties
N2O4
Molar mass 92.010 g·mol−1
Appearance Colourless liquid, orange gas
Density 1.44246 g/cm3 (liquid, 21 °C)
Melting point −11.2 °C (11.8 °F; 261.9 K) and decomposes to NO2
Boiling point 21.69 °C (71.04 °F; 294.84 K)
Reacts to form nitrous and nitric acids
Vapor pressure 96 kPa (20 °C)[1]
−23.0·10−6 cm3/mol
1.00112
Structure
Planar, D2h
small, non-zero
Thermochemistry
304.29 J/K⋅mol[2]
+9.16 kJ/mol[2]
Hazards
GHS labelling:
GHS03: OxidizingGHS04: Compressed GasGHS05: CorrosiveGHS06: ToxicGHS07: Exclamation mark
Danger
H270, H280, H314, H330, H335, H336
P220, P244, P260, P261, P264, P271, P280, P284, P301+P330+P331, P303+P361+P353, P304+P340, P305+P351+P338, P310, P312, P320, P321, P363, P370+P376, P403, P403+P233, P405, P410+P403, P501
NFPA 704 (fire diamond)
[3][4]
NFPA 704 four-colored diamond
4
0
0
OX
Flash point Non-flammable
Safety data sheet (SDS) External SDS
Related compounds
Related compounds
Except where otherwise noted, data are given for materials in their standard state (at 25 °C [77 °F], 100 kPa).
☒N verify (what is checkY☒N ?)
Infobox references

Dinitrogen tetroxide, commonly referred to as nitrogen tetroxide (NTO), and occasionally (usually among ex-USSR/Russia rocket engineers) as amyl, is the chemical compound N2O4. It is a useful reagent in chemical synthesis. It forms an equilibrium mixture with nitrogen dioxide. Its molar mass is 92.011 g/mol.

Dinitrogen tetroxide is a powerful oxidizer that is hypergolic (spontaneously reacts) upon contact with various forms of hydrazine, which has made the pair a common bipropellant for rockets.

Structure and properties

Dinitrogen tetroxide could be regarded as two nitro groups (-NO2) bonded together. It forms an equilibrium mixture with nitrogen dioxide.[5] The molecule is planar with an N-N bond distance of 1.78 Å and N-O distances of 1.19 Å. The N-N distance corresponds to a weak bond, since it is significantly longer than the average N-N single bond length of 1.45 Å.[6] This exceptionally weak σ bond (amounting to overlapping of the sp2 hybrid orbitals of the two NO2 units[7]) results from the simultaneous delocalization of the bonding electron pair across the whole N2O4 molecule, and the considerable electrostatic repulsion of the doubly occupied molecular orbitals of each NO2 unit.[8]

Unlike NO2, N2O4 is diamagnetic since it has no unpaired electrons.[9] The liquid is also colorless but can appear as a brownish yellow liquid due to the presence of NO2 according to the following equilibrium:

N2O4 ⇌ 2 NO2

Higher temperatures push the equilibrium towards nitrogen dioxide. Inevitably, some dinitrogen tetroxide is a component of smog containing nitrogen dioxide.

Production

Nitrogen tetroxide is made by the catalytic oxidation of ammonia: steam is used as a diluent to reduce the combustion temperature. In the first step, the ammonia is oxidized into nitric oxide:

4 NH3 + 5 O2 → 4 NO + 6 H2O

Most of the water is condensed out, and the gases are further cooled; the nitric oxide that was produced is oxidized to nitrogen dioxide, which is then dimerized into nitrogen tetroxide:

2 NO + O2 → 2 NO2
2 NO2 ⇌ N2O4

and the remainder of the water is removed as nitric acid. The gas is essentially pure nitrogen dioxide, which is condensed into dinitrogen tetroxide in a brine-cooled liquefier.[10]

Dinitrogen tetroxide can also be made through the reaction of concentrated nitric acid and metallic copper. This synthesis is practical in a laboratory setting. Dinitrogen tetroxide can also be produced by heating metal nitrates.[11] The oxidation of copper by nitric acid is a complex reaction forming various nitrogen oxides of varying stability which depends on the concentration of the nitric acid, presence of oxygen, and other factors. The unstable species further react to form nitrogen dioxide which is then purified and condensed to form dinitrogen tetroxide.

Use as a rocket propellant

Nitrogen tetroxide is used as an oxidizing agent in one of the most important rocket propellant systems because it can be stored as a liquid at room temperature. Pedro Paulet, a Peruvian polymath, reported in 1927 that he had experimented in the 1890s with a rocket engine that used spring-loaded nozzles that periodically introduced vaporized nitrogen tetroxide and a petroleum benzine to a spark plug for ignition, with the engine putting out 300 pulsating explosions per minute.[12][13] Paulet would go on to visit the German rocket association Verein für Raumschiffahrt (VfR) and on March 15, 1928, Valier applauded Paulet's liquid-propelled rocket design in the VfR publication Die Rakete, saying the engine had "amazing power".[14] Paulet would soon be approached by Nazi Germany to help develop rocket technology, though he refused to assist and never shared the formula for his propellant.[15]

In early 1944, research on the usability of dinitrogen tetroxide as an oxidizing agent for rocket fuel was conducted by German scientists, although the Germans only used it to a very limited extent as an additive for S-Stoff (fuming nitric acid). It became the storable oxidizer of choice for many rockets in both the United States and USSR by the late 1950s. It is a hypergolic propellant in combination with a hydrazine-based rocket fuel. One of the earliest uses of this combination was on the Titan family of rockets used originally as ICBMs and then as launch vehicles for many spacecraft. Used on the U.S. Gemini and Apollo spacecraft and also on the Space Shuttle, it continues to be used as station-keeping propellant on most geo-stationary satellites, and many deep-space probes. It is also the primary oxidizer for Russia's Proton rocket.

When used as a propellant, dinitrogen tetroxide is usually referred to simply as nitrogen tetroxide and the abbreviation NTO is extensively used. Additionally, NTO is often used with the addition of a small percentage of nitric oxide, which inhibits stress-corrosion cracking of titanium alloys, and in this form, propellant-grade NTO is referred to as mixed oxides of nitrogen (MON). Most spacecraft now use MON instead of NTO; for example, the Space Shuttle reaction control system used MON3 (NTO containing 3% NO by weight).[16]

The Apollo-Soyuz mishap

On 24 July 1975, NTO poisoning affected three U.S. astronauts on the final descent to Earth after the Apollo-Soyuz Test Project flight. This was due to a switch accidentally left in the wrong position, which allowed the attitude control thrusters to fire after the cabin fresh air intake was opened, allowing NTO fumes to enter the cabin. One crew member lost consciousness during descent. Upon landing, the crew was hospitalized for five days for chemical-induced pneumonia and edema.[17][18]

Power generation using N2O4

The tendency of N2O4 to reversibly break into NO2 has led to research into its use in advanced power generation systems as a so-called dissociating gas.[19] "Cool" dinitrogen tetroxide is compressed and heated, causing it to dissociate into nitrogen dioxide at half the molecular weight. This hot nitrogen dioxide is expanded through a turbine, cooling it and lowering the pressure, and then cooled further in a heat sink, causing it to recombine into nitrogen tetroxide at the original molecular weight. It is then much easier to compress to start the entire cycle again. Such dissociative gas Brayton cycles have the potential to considerably increase efficiencies of power conversion equipment.[20]

The high molecular weight and smaller volumetric expansion ratio of nitrogen dioxide compared to steam allows the turbines to be more compact.[21]

N2O4 was the main component of the "nitrin" working fluid in the decommissioned Pamir-630D portable nuclear reactor which operated from 1985 to 1987.[22]

Chemical reactions

Intermediate in the manufacture of nitric acid

Nitric acid is manufactured on a large scale via N2O4. This species reacts with water to give both nitrous acid and nitric acid:

N2O4 + H2O → HNO2 + HNO3

The coproduct HNO2 upon heating disproportionates to NO and more nitric acid. When exposed to oxygen, NO is converted back into nitrogen dioxide:

2 NO + O2 → 2 NO2

The resulting NO2 and N2O4 can be returned to the cycle to give the mixture of nitrous and nitric acids again.

Synthesis of metal nitrates

N2O4 undergoes molecular autoionization to give [NO+] [NO3−], with the former nitrosonium ion being a strong oxidant. Various anhydrous transition metal nitrate complexes can be prepared from N2O4 and base metal.[23]

2 N2O4 + M → 2 NO + M(NO3)2

where M = Cu, Zn, or Sn.

If metal nitrates are prepared from N2O4 in completely anhydrous conditions, a range of covalent metal nitrates can be formed with many transition metals. This is because there is a thermodynamic preference for the nitrate ion to bond covalently with such metals rather than form an ionic structure. Such compounds must be prepared in anhydrous conditions, since the nitrate ion is a much weaker ligand than water, and if water is present the simple nitrate of the hydrated metal ion will form. The anhydrous nitrates concerned are themselves covalent, and many, e.g. anhydrous copper nitrate, are volatile at room temperature. Anhydrous titanium nitrate sublimes in vacuum at only 40 °C. Many of the anhydrous transition metal nitrates have striking colours. This branch of chemistry was developed by Cliff Addison and Norman Logan at the University of Nottingham in the UK during the 1960s and 1970s when highly efficient desiccants and dry boxes started to become available.

References

  1. ↑ International Chemical Safety Card https://www.ilo.org/dyn/icsc/showcard.display?p_lang=en&p_card_id=0930&p_version=2
  2. 1 2 P.W. Atkins and J. de Paula, Physical Chemistry (8th ed., W.H. Freeman, 2006) p.999
  3. ↑ "Chemical Datasheet: Nitrogen tetroxide". CAMEO Chemicals NOAA. Retrieved 8 September 2020.
  4. ↑ "Compound Summary: Dinitrogen tetroxide". PubChem. Retrieved 8 September 2020.
  5. ↑ Bent, Henry A. (1963). "Dimers of Nitrogen Dioxide. II. Structure and Bonding". Inorganic Chemistry. 2 (4): 747–752. doi:10.1021/ic50008a020.
  6. ↑ Petrucci, Ralph H.; Harwood, William S.; Herring, F. Geoffrey (2002). General chemistry: principles and modern applications (8th ed.). Upper Saddle River, N.J: Prentice Hall. p. 420. ISBN 978-0-13-014329-7. LCCN 2001032331. OCLC 46872308.
  7. ↑ Rayner-canham, Geoff (2013). Descriptive inorganic chemistry (6th ed.). p. 400. ISBN 978-1-319-15411-0. OCLC 1026755795.
  8. ↑ Ahlrichs, Reinhart; Keil, Frerich (1974-12-01). "Structure and bonding in dinitrogen tetroxide (N2O4)". Journal of the American Chemical Society. 96 (25): 7615–7620. doi:10.1021/ja00832a002. ISSN 0002-7863.
  9. ↑ Holleman, A. F.; Wiberg, E. "Inorganic Chemistry" Academic Press: San Diego, 2001. ISBN 978-0-12-352651-9.
  10. ↑ Hebry, TH; Inskeep, GC (1954). Modern Chemical Processes: A Series of Articles Describing Chemical Manufacturing Plants. New York: Reinhold. p. 219.
  11. ↑ Rennie, Richard (2016). A Dictionary of Chemistry. Oxford University Press. p. 178. ISBN 978-0-19-872282-3.
  12. ↑ Gonzales Obando, Diana (2021-07-22). "Pedro Paulet: el genio peruano que se adelantó a su época y fundó la era espacial". El Comercio (in Spanish). Retrieved 2022-03-13.
  13. ↑ "Un peruano Pedro Paulet reclama la propiedad de su invento". El Comercio (in Spanish). 25 August 1927. Retrieved 2022-03-13.
  14. ↑ Mejía, Álvaro (2017). Pedro Paulet, sabio multidisciplinario (in Spanish). Universidad Católica San Pablo. pp. 95–122.
  15. ↑ "El peruano que se convirtió en el padre de la astronáutica inspirado por Julio Verne y que aparece en los nuevos billetes de 100 soles". BBC News (in Spanish). Retrieved 2022-03-11.
  16. ↑ "Rocket Propellant Index". Archived from the original on 2008-05-11. Retrieved 2005-03-01.
  17. ↑ "Brand Takes Blame For Apollo Gas Leak", Florence, AL - Times Daily newspaper, August 10, 1975
  18. ↑ Sotos, John G., MD. "Astronaut and Cosmonaut Medical Histories", May 12, 2008, accessed April 1, 2011.
  19. ↑ Stochl, Robert J. (1979). Potential performance improvement by using a reacting gas (nitrogen tetroxide) as the working fluid in a closed Brayton cycle (PDF) (Technical report). NASA. TM-79322.
  20. ↑ Ragheb, R. "Nuclear Reactors Concepts and Thermodynamic Cycles" (PDF). Retrieved 1 May 2013.
  21. ↑ Binotti, Marco; Invernizzi, Costante M.; Iora, Paolo; Manzolini, Giampaolo (March 2019). "Dinitrogen tetroxide and carbon dioxide mixtures as working fluids in solar tower plants". Solar Energy. 181: 203–213. doi:10.1016/j.solener.2019.01.079. S2CID 104462066.
  22. ↑ Paliukhovich, V.M. (7 May 2023). "Safe Decommissioning of Mobile Nuclear Power Plant" (PDF). International Atomic Energy Agency. Minsk, Belarus: Department for Supervision of Industrial and Nuclear Safety. Archived (PDF) from the original on 7 May 2023. Retrieved 7 May 2023.
  23. ↑ Addison, C. Clifford (February 1980). "Dinitrogen tetroxide, nitric acid, and their mixtures as media for inorganic reactions". Chemical Reviews. 80 (1): 21–39. doi:10.1021/cr60323a002.
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