Results 201 to 210 of about 327,422 (252)
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Surface Energy and Crystallization Phenomena of Ammonium Dinitramide

Propellants, Explosives, Pyrotechnics, 2005
AbstractAmmonium dinitramide (ADN) was characterized during recrystallization from the melt. The surface tension of molten ADN at 97 °C was measured to be 89 mN/m. The wetting angles between molten ADN and different solid surfaces (polytetrafluoroethylene, glass, steel, and aluminum) were determined.
Ulrich Teipel, Thomas Heintz
openaire   +1 more source

Comparative study on detonation parameters of ammonium dinitramide and ammonium perchlorate in composite explosives

Journal of Energetic Materials
Ammonium dinitramide (ADN) has the advantages of chlorine free, low characteristic signal and high energy compared with ammonium perchlorate (AP), which is the most likely oxidant to replace ammonium perchlorate.
Wenxiang Bian   +3 more
semanticscholar   +1 more source

Integrative oncology: Addressing the global challenges of cancer prevention and treatment

Ca-A Cancer Journal for Clinicians, 2022
Jun J Mao,, Msce   +2 more
exaly  

Effect of typical copper-based catalysts on the thermolysis and combustion behavior of high-energy oxidant ammonium dinitramide

Journal of Thermal Analysis and Calorimetry
Fuyao Chen   +7 more
semanticscholar   +1 more source

Effect of ammonium nitrate doping on the low-temperature thermal stability of ammonium dinitramide

Journal of Thermal Analysis and Calorimetry
Yuanlu Cui   +3 more
semanticscholar   +1 more source

Reducing Preheating Requirements for 1-N-Scale Thruster with Ammonium Dinitramide-H2O2 Monopropellant

Journal of Propulsion and Power
J. Kim   +4 more
semanticscholar   +1 more source

Hydroxyl-Terminated Polybutadiene (HTPB) Composite Propellant with Different Ammonium Dinitramide (ADN) Contents: Combustion and Aluminum Agglomeration

Combustion Science and Technology
Kai Xin   +9 more
semanticscholar   +1 more source

Rheological properties and propulsion performance of an ammonium dinitramide-based gel propellant with sustainable reignition and adjustable thrust flexibility

Acta Astronautica
Jingyuan Zhang   +9 more
semanticscholar   +1 more source

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