Trinitramide

Trinitramide

Structural formula of trinitramide Space-filling model of trinitramide
Names
IUPAC name N,N-Dinitronitramide
Other names Trinitroamine Trinitroammonia
Identifiers
CAS Number	113282-38-5 checkY
3D model (JSmol)	Interactive image Interactive image
ChemSpider	24751851 checkY
ECHA InfoCard
E number
PubChem CID	57459337
CompTox Dashboard (EPA)	{{#property:P3117}}
InChI InChI=1S/N4O6/c5-2(6)1(3(7)8)4(9)10 checkY Key: LZLKDWBQTGTOQY-UHFFFAOYSA-N checkY
SMILES O=N(=O)N(N(=O)=O)N(=O)=O N([N+](=O)[O-])([N+](=O)[O-])[N+](=O)[O-]
Properties
Chemical formula	N(NO2)3
Molar mass	152.022 g·mol−1
Related compounds
Related compounds	Ammonia Nitramide Dinitramide Dinitrogen pentoxide Tetranitromethane Nitroformate
Except where otherwise noted, data are given for materials in their standard state (at 25 °C [77 °F], 100 kPa). checkY verify (what is checkY☒N ?) Infobox references

Trinitramide is a compound of nitrogen and oxygen with the molecular formula N(NO₂)₃. The compound was detected and described in 2010 by researchers at the Royal Institute of Technology (KTH) in Sweden. It is made of a nitrogen atom bonded to three nitro groups (−NO₂).

Earlier, there had been speculation whether trinitramide could exist. Theoretical calculations by Montgomery and Michels in 1993 showed that the compound was likely to be stable.

Preparation

Trinitramide is prepared by the nitration reaction of either potassium dinitramide or ammonium dinitramide with nitronium tetrafluoroborate in acetonitrile at low temperatures.

[NH₄]⁺[N(NO₂)₂]⁻ + [NO₂]⁺[BF₄]⁻ → N(NO₂)₃ + [NH₄]⁺[BF₄]⁻

Uses

Trinitramide has a potential use as one of the most efficient and least polluting of rocket propellant oxidizers, as it is chlorine-free. This is potentially an important development, because the Tsiolkovsky rocket equation implies that even small improvements in specific impulse yields a similar change in delta-v, which can make large improvements in the size of practical rocket launch payloads. The density impulse (impulse per volume) of a trinitramide based propellant could be 20 to 30 percent better than most existing formulations, however the specific impulse (impulse per mass) of formulations with liquid oxygen is higher.