4.7 Article

Pyrolytic Decomposition of Ammonia Borane to Boron Nitride

Journal

INORGANIC CHEMISTRY
Volume 50, Issue 3, Pages 783-792

Publisher

AMER CHEMICAL SOC
DOI: 10.1021/ic101020k

Keywords

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Funding

  1. Ensign-Bickford Aerospace & Defense Company [W909MY-06-0041, W15P7T-07-C-P420]
  2. Department of Energy, Office of Basic Energy Sciences, Division of Chemical, Geochemical, and Biological Scences
  3. U.S. Army CECOM ACQ Center

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The thermal decomposition of ammonia borane was studied using a variety of methods to qualitatively identify gas and remnant solid phase species after thermal treatments up to 1500 degrees C. At about 110 degrees C, ammonia borane begins to decompose yielding H-2 as the major gas phase product. A two step decomposition process leading to a polymeric -[NH=BH](n)- species above 130 degrees C is generally accepted. In this comprehensive study of decomposition pathways, we confirm the first two decomposition steps and identify a third process initiating at 1170 degrees C which leads to a semicrystalline hexagonal phase boron nitride. Thermogravimetric analysis (TGA) was used to identify the onset of the third step. Temperature programmed desorption-mass spectroscopy (TPD-MS) and vacuum line methods identify molecular aminoborane (H2N=BH2) as a species that can be released in appreciable quantities with the other major impurity, borazine. Attenuated total reflectance Fourier transform infrared spectroscopy (ATR-FTIR) was used to identify the chemical states present in the solid phase material after each stage of decomposition. The boron nitride product was examined for composition, structure, and morphology using scanning Auger microscopy (SAM), powder X-ray diffraction (XRD), and field emission scanning electron microscopy (FESEM). Thermogravimetric Analysis-Mass Spectroscopy (TGA-MS) and Differential Scanning Calorimetry (DSC) were used to identify the onset temperature of the first two mass loss events.

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