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High performance microthruster with ammonium-dinitramide-based monopropellant
A high performance environmentally friendly ammonium dinitramide (ADN) based liquid monopropellant was used to develop a thruster with improved performance compared to a conventional hydrogen peroxide propellant microthruster.
Kyu-Seop Kim, Sejin Kwon
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Thermal decomposition of ammonium dinitramide and mechanism of anomalous decay of dinitramide salts
Russian Chemical Bulletin, 1999Thermal decomposition of ammonium dinitramide proceedsvia homolytic rupture of the N−NO2 bond and partially by the proton transfer reaction. The monomolecular decay of the anion to N2O and NO3 − in the solid state at 60 °C occurs with higher rates than those in the melt.
A. N. Pavlov +4 more
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New technologies for ammonium dinitramide based monopropellant thrusters – The project RHEFORM
New technologies are developed in the project RHEFORM to enable the replacement of hydrazine with liquid propellants based on ammonium dinitramide (ADN).
Christian Hendrich +2 more
exaly +2 more sources
Stabilization of ammonium dinitramide in the liquid phase
Russian Chemical Bulletin, 2000The kinetics of accumulation of the main products of thermal decomposition of ammonium dinitramide in the melt was investigated. The isotope composition of nitrogen-containing gases evolved by the decomposition of 15NH4N(NO2)2 and NH4 15N(NO2)2 was found.
A. B. Andreev +4 more
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Combustion of ammonium dinitramide/polycaprolactone propellants
Proceedings of the Combustion Institute, 2002This paper is devoted to the investigation of characteristics and mechanisms of combustion of a compositesolid rocket pseudo-propellant of stoichiometric composition based on ammonium dinitramide (ADN) and polycaprolactone (PCL). Experimental data on the dependence of burning rate on pressure in the pressure range of 4–8 MPa for the ADN/PCL propellant ...
O.P. Korobeinichev +3 more
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Role of Additives in the Combustion of Ammonium Dinitramide
Propellants, Explosives, Pyrotechnics, 2014AbstractThe thermal decomposition behavior and combustion characteristics of mixtures of ammonium dinitramide (ADN) with additives were studied. Micrometer‐sized particles of Al, Fe2O3, TiO2, NiO, Cu(OH)NO3, copper, CuO, and nanometer‐sized particles of aluminum (Alex) and CuO (nano‐CuO) were employed.
Koji Fujisato +4 more
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Ammonium Dinitramide: Kinetics and Mechanism of Thermal Decomposition
The Journal of Physical Chemistry A, 1997Thermal decomposition of ammonium dinitramide (ADN) has been studied by differential scanning calorimetry (DSC) and thermal gravimetry combined with mass spectrometry (TG−MS). ADN decomposes in the range 130−230 °C with an overall heat release of 240 ± 40 kJ mol-1.
Sergey Vyazovkin, Charles A. Wight
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On the mechanism of thermal decomposition of ammonium dinitramide (review)
Combustion, Explosion, and Shock Waves, 2016Despite significant progress in studying thermal decomposition of ammonium dinitramide (ADN), the kinetics of the process at the level of elementary stages has not been adequately understood. The aim of this review is to summarize various published data, which are of interest for studying and simulating the processes of thermal decomposition and ...
N. E. Ermolin, V. M. Fomin
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Ammonium Dinitramide−Water: Interaction and Properties
Journal of Chemical & Engineering Data, 2006The interaction between ammonium dinitramide (ADN) and water was experimentally investigated by determining the solid−liquid phase diagram for the system ADN−water and by measuring its critical relative humidity at 25 °C. Additionally, the density of aqueous ADN solutions of different compositions were measured in the temperature range from (5 to 85 ...
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Thermal Decomposition and Combustion of Ammonium Dinitramide (Review)
Combustion, Explosion and Shock Waves, 2005A comprehensive review of thermal decomposition and combustion of ammonium dinitramide (ADN) has been conducted. The basic thermal properties, chemical pathways, and reaction products in both the condensed and gas phases are analyzed over a broad range of ambient conditions.
R. Yang, P. Thakre, V. Yang
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