Ammonium dinitramide
Structural formula | |||||||||||||||||||
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General | |||||||||||||||||||
Surname | Ammonium dinitramide | ||||||||||||||||||
Molecular formula | H 4 N 4 O 4 | ||||||||||||||||||
Brief description |
Colorless crystals |
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properties | |||||||||||||||||||
Molar mass | 124.06 g mol −1 | ||||||||||||||||||
Physical state |
firmly |
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density |
1.812 g cm −3 (20 ° C) |
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Melting point |
92 ° C (decomposition from 135 ° C) |
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safety instructions | |||||||||||||||||||
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As far as possible and customary, SI units are used. Unless otherwise noted, the data given apply to standard conditions . |
Ammonium dinitramide (ADN) is of great importance as an oxidizer for fuels and as an explosive . ADN was first developed in the Soviet Union ( Vladimir Alexandrowitsch Tartakowski and others) and was known in the West after the Cold War .
properties
Ammonium dinitramide consists of solid, colorless crystals . It is still difficult to keep the material pure.
Explosion parameters
Important explosion indicators are:
- Heat of explosion : 2668 kJ kg −1 (H 2 O (g)) .
- Normal gas volume : 1084 l kg −1 .
- Specific energy : 843 kJ kg −1
- Impact sensitivity : 4 N · m
- Friction sensitivity : 64 N
use
Ammonium dinitramide is a solid oxidizer mainly used for high performance multicomponent solid rocket propellants . ADN and other similar compounds are the subject of several patents for use as multicomponent solid rocket propellants and as explosives , both for pyrotechnic uses in general and for other uses such as means for inflating airbags . Due to its good oxygen balance and high enthalpy of formation, ADN appears to be of interest as a halogen-free oxidizing agent for solid rocket propellants and is currently the subject of intensive studies. The absence of halogens makes radar detection of the rocket's exhaust gas difficult .
It is also part of the monergole liquid fuel mixture LMP-103S for satellite engines . This could replace the much more toxic hydrazine as monergolic fuel for spacecraft.
Manufacturing
Ammonium dinitramide is obtained by ammonolysis of dinitroamines , which are formed by stepwise nitration of urethanes , β, β-iminodipropionitrile or nitramide . The last nitration stage in each case requires the strongest nitration reagents such as nitronium tetrafluoroborate or dinitrogen pentoxide . Another process leads via the direct nitration of ammonia with nitrous oxide to a product mixture of ADN and ammonium nitrate .
Individual evidence
- ↑ Venkatachalam, S .; Santhosh, G .; Ninan, KN: An Overview on the Synthetic Routes and Properties of Ammonium Dinitramide (ADN) and other Dinitramide Salts in Propellants, Explosives, Pyrotechnics 29 (2004) 178-187, doi : 10.1002 / prep.200400043 .
- ↑ a b c d e f g Koehler, J .; Meyer, R .; Homburg, A .: Explosivstoffe , tenth, completely revised edition. Wiley-VCH, Weinheim 2008, ISBN 978-3-527-32009-7 .
- ↑ This substance has either not yet been classified with regard to its hazardousness or a reliable and citable source has not yet been found.
- ↑ patent DE10201937 .
- ↑ Patent EP0001390323 : AMMONIUM DINITRAMIDE BASED LIQUID SINGLE-COMPONENT PROPELLER WITH IMPROVED COMBUSTION STABILITY AND STORAGE LIFE
- ^ Science Online
- ^ 'Green' satellite fuel designed to make space safer. ESA, March 16, 2010, accessed July 9, 2011 .
- ↑ J. Köhler, Rudolf Meyer, Axel Homburg: Explosivstoffe. 9., revised. u. exp. A., Wiley, 1998, ISBN 3527288643 ( excerpt ).