A process was developed to recover boron from the chemicals of an old propulsion engine. The pellet igniter in a propulsion engine is composed of oxidizers, boron compounds and binders. In order to extract the boron compounds, an organic solvent and/or aqueous treatments were employed and followed by a sintering process. A qualitative and quantitative characterization of boron was performed by differential scanning calorimeter and thermogravimetric analyses (DSC-TGA), X-ray diffractometer (XRD), X-ray fluorescence (XRF), inductively coupled plasma (ICP) and scanning electron microscopy coupled with energy-dispersive X-ray spectroscopy (SEM–EDX). Overall, 79.7% of boron recovery was achieved. The final purity level of boron was 94%, which is sufficiently pure to satisfy the US Military’s specifications (US-MIL-P-46994B) for the pellet igniter. From the pellets igniter (a), boron (b) and potassium nitrate (c) are purely separated.
Read full abstract