In situ time-resolved Raman spectroscopy of nitromethane under static and dynamic compression

Author:

Chaurasia S.1ORCID,Mohan Ashutosh23ORCID,Mishra Ajay K.23ORCID,Sijoy C. D.34ORCID,Mishra V.34ORCID

Affiliation:

1. School of Mathematics and Physics, Queen's University Belfast 1 , BT7 1NN, United Kingdom

2. High Pressure & Synchrotron Radiation Physics Division, Bhabha Atomic Research Centre 2 , Mumbai 400085, India

3. Homi Bhabha National Institute 3 , Mumbai 400094, India

4. Computational Analysis Division, Bhabha Atomic Research Centre 4 , Visakhapatnam 531011, India

Abstract

Energetic materials are extensively used as propellants in rockets demanding the understanding of their chemical and thermal stability for safe storage and transportation as well as ease of decomposition. Nitromethane (NM) is one such material with significant performance advantage over other mono propellants. In this manuscript, we report the detailed molecular-level behavior of NM under static and dynamic compression. Dynamic compression experiments were performed up to ∼6.4 GPa using a 2 J/8 ns Nd: YAG laser coupled with time-resolved Raman spectroscopy (TRRS) setup. Static compression experiments were performed up to ∼20 GPa using a diamond anvil cell. During laser-driven shock compression, NM undergoes three phase transitions at 1.1, 2.5, and 3.4 GPa. However, in the case of static compression, the corresponding phase transitions were observed at 0.3, 1.3–1.8, and 2.5 GPa. TRRS was also performed at 300 mJ (1.47 GW/cm2), 500 mJ (2.45 GW/cm2), and 800 mJ (3.9 GW/cm2) and intensity ratios of shocked and un-shocked Raman peaks were utilized to experimentally calculate the shock velocities, which were determined to be 2.66 ± 0.09, 3.58 ± 0.40, and 3.83 ± 0.60 km/s, respectively. These experimental results were corroborated with the one-dimensional (1D) radiation hydrodynamics simulations, performed to obtain shock pressure. The shock velocities at these laser intensities were calculated to be 2.98, 3.69, and 3.92 km/s, respectively, which are in reasonably close agreement with our observed results.

Publisher

AIP Publishing

Subject

General Physics and Astronomy

Reference57 articles.

1. J. Eric Boyer , “Combustion characteristics and flame structure of NM liquid monopropellant,” Ph.D. thesis (The Pennsylvania State University, 2005).

2. Detonation on a tabletop: Nitromethane with high time and space resolution;J. Appl. Phys.,2018

3. The structure of nitromethane at pressures of 0.3 to 6.0 GPa;J. Phys. Chem.,1985

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