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Other names
hydroxylamine nitrate
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Identifiers | |
3D model (JSmol)
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ChemSpider | |
ECHA InfoCard | 100.033.342 |
EC Number |
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PubChem CID
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CompTox Dashboard (EPA)
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Properties | |
[NH3OH]+[NO3]− | |
Molar mass | 96.04 g/mol |
Density | 1.84 g/cm3 |
Melting point | 48 °C |
Soluble | |
Hazards | |
GHS labelling: | |
Danger | |
H201, H302, H311, H315, H317, H319, H351, H373, H400 | |
P201, P202, P210, P230, P240, P250, P260, P261, P264, P270, P272, P273, P280, P281, P301+P312, P302+P352, P305+P351+P338, P308+P313, P312, P314, P321, P322, P330, P332+P313, P333+P313, P337+P313, P361, P362, P363, P370+P380, P372, P373, P391, P401, P405, P501 | |
Safety data sheet (SDS) | External MSDS (as 18 % solution) |
Related compounds | |
Other anions
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Hydroxylammonium sulfate Hydroxylammonium chloride |
Other cations
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Ammonium nitrate |
Related compounds
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Hydroxylamine |
Except where otherwise noted, data are given for materials in their standard state (at 25 °C [77 °F], 100 kPa).
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Hydroxylammonium nitrate or hydroxylamine nitrate (HAN) is an inorganic compound with the chemical formula [NH3OH]+[NO3]−. It is a salt derived from hydroxylamine and nitric acid. In its pure form, it is a colourless hygroscopic solid. It has potential to be used as a rocket propellant either as a solution in monopropellants or bipropellants.[1] Hydroxylammonium nitrate (HAN)-based propellants are a viable and effective solution for future green propellant-based missions, as it offers 50% higher performance for a given propellant tank compared to commercially used hydrazine.