Data on the optical combustion properties of ammonium dinitramide (ADN) systems as powerful oxidants for propellants and explosives are given from expts. using ADN mixed with paraffin in a mass ratio of 90:10 corresponding to a max. specific impulse. Burning rates of 50 mm/s were measured at 7 MPa and a pressure exponent of 0.8 was detd. Spectroscopic investigations yield to flame temps. in the range of the adiabatic flame temp. of 2960 K and give first hints to the chem. reaction mechanism of the ADN combustion with hydrocarbons
This paper discusses results obtained by studying a row of progressively complicated ammonium-nitrat...
Ammonium dinitramide/glycidyl azide polymer (ADN/GAP) composite propellants with or without metallic...
Mechanistic pathways for the thermal decompn. of the solid-state energetic oxidizers ammonium dinitr...
Ammonium dinitramide [NH4N(NO2)2, ADN] is considered as a possible replacement for ammonium perchlor...
In recent years the awareness of the environmental risks associated with the use of ammonium perchlo...
Solid rocket propellants based on ammonium dinitramide (ADN) as oxidizer and glycidyl azide polymer ...
ADN (ammonium dinitramide) is seen as possible replacement oxidizer for ammonium perchlorate in rock...
Ammonium dinitramide (ADN), NH4N(NO2)2, a new energetic compd. was investigated as a potential repla...
Thermal properties and decompn. behavior of the new energetic material ammonium dinitramide (ADN) we...
Solid rocket propellants based on ammonium dinitramide (ADN) as oxidizer and glycidyl azide polymer ...
Plasma-enhanced decomposition is a promising method to achieve reliable ignition and better thruster...
EP 1331213 A UPAB: 20040205 NOVELTY - Production of additive-modified ammonium dinitramide (ADN) inv...
The detonation curvature and detonation velocity of melt cast Ammonium Dinitramide, or ADN (NH4N(NO2...
Solid rocket motors are today the most cost effective, competitive and reliable propulsion technolog...
The thermal decomposition of ammonium dinitramide (ADN) and potassium dinitramide (KDN) were examine...
This paper discusses results obtained by studying a row of progressively complicated ammonium-nitrat...
Ammonium dinitramide/glycidyl azide polymer (ADN/GAP) composite propellants with or without metallic...
Mechanistic pathways for the thermal decompn. of the solid-state energetic oxidizers ammonium dinitr...
Ammonium dinitramide [NH4N(NO2)2, ADN] is considered as a possible replacement for ammonium perchlor...
In recent years the awareness of the environmental risks associated with the use of ammonium perchlo...
Solid rocket propellants based on ammonium dinitramide (ADN) as oxidizer and glycidyl azide polymer ...
ADN (ammonium dinitramide) is seen as possible replacement oxidizer for ammonium perchlorate in rock...
Ammonium dinitramide (ADN), NH4N(NO2)2, a new energetic compd. was investigated as a potential repla...
Thermal properties and decompn. behavior of the new energetic material ammonium dinitramide (ADN) we...
Solid rocket propellants based on ammonium dinitramide (ADN) as oxidizer and glycidyl azide polymer ...
Plasma-enhanced decomposition is a promising method to achieve reliable ignition and better thruster...
EP 1331213 A UPAB: 20040205 NOVELTY - Production of additive-modified ammonium dinitramide (ADN) inv...
The detonation curvature and detonation velocity of melt cast Ammonium Dinitramide, or ADN (NH4N(NO2...
Solid rocket motors are today the most cost effective, competitive and reliable propulsion technolog...
The thermal decomposition of ammonium dinitramide (ADN) and potassium dinitramide (KDN) were examine...
This paper discusses results obtained by studying a row of progressively complicated ammonium-nitrat...
Ammonium dinitramide/glycidyl azide polymer (ADN/GAP) composite propellants with or without metallic...
Mechanistic pathways for the thermal decompn. of the solid-state energetic oxidizers ammonium dinitr...