Astrochemistry and combustion studies with shock waves
Abstract
Shockwaves and polycyclic aromatic hydrocarbons (PAHs) are ubiquitous in
the interstellar medium (ISM) and on Earth. Combustion chemistry provides
the fundamental reaction routes and mechanisms for PAH formation. These
fundamental chemical principles governing hydrocarbon combustion can be
utilized to describe the formation and destruction of PAHs in astrophysical
environments under similar shocked environments.
The primary focus of my thesis is PAHs, specifically examining the thermal
processing of PAHs through shock waves in astrochemistry and the formation
of aromatics, which eventually form PAHs during the pyrolysis of hydrocarbons
in combustion experiments. The formation and breakdown of PAHs are assisted
by shockwaves under well-defined reaction times, high temperatures, and highpressure
conditions generated via shock tube facilities. Home-built shock tube
facilities in the Laboratory for Hypersonic and Shockwave Research (LHSR) lab
were used to investigate high-temperature chemical kinetics and spectroscopy
experiments relevant to astrochemistry and combustion. The ’single pulse
nature’ in the shock tube causes the reflected shock to increase the temperature
up to ∼6000 K for ∼2-3 ms of dwell time. The molecules are heated behind the
reflected shock wave through collisions that facilitate energy transfer between
the driver gas, argon, and the sample molecule, while the wall of the shock
tube remains at an ambient temperature.
Chapter 01 explores the occurrence of PAHs both on Earth and in space,
highlighting the significance and justification for investigating PAHs in the pyrolysis
of both hydrindane and methylcyclopentane. Chapter 02 examines the
specifics of the shock tube facilities, emission spectroscopy tools, gas chrovi
matography instruments, and the computational methodologies used in this
thesis.
For the astrochemistry experiments discussed in Chapter 03, a new Material
Shock Tube (MST) facility was established with an optical access chamber
focusing on time-resolved and time-integrated emission spectroscopy in the
UV-Vis-NIR region. The processing of interstellar dust analogues, including
PAHs and fullerenes, via UV irradiation or ion/electron bombardment has been
extensively studied; however, investigations through shock processing remain
limited. The prototypical PAH coronene (C24H12) was selected for the shock
processing study with a focus on the C2 (Swan band) time-resolved emissions
in the UV-vis region. Key findings from the research show that the shock
waves enable the conversion of polycyclic aromatic PAHs into smaller hydrocarbons
CnHx, a potential DIB carrier, and carbon clusters that subsequently
recombine during the cooling phase into graphene-like structures, affecting the
carbon lifecycle of the interstellar medium. The identification of CnHx (where
n = 3–9 with a predominance of odd-numbered n, and x = 1–3) species as
potential carriers of a broad green emission seen in the laboratory suggests a
possible link to the 5450 ˚A diffuse interstellar band (DIB). The results were
supported by the collection and analysis of solid residues post-shock, as well
as molecular dynamics (MD) simulations conducted by various collaborators.
This study establishes a foundation for future research focused on understanding
the complex interactions among PAH and shocks, as well as the evolution
of carbonaceous materials in the interstellar medium.
The second section of my thesis is related to combustion experiments conducted
in the shock tube, as discussed in Chapters 04 and 05. For combustion
experiments, the existing Chemical Shock Tube (CST) facility was modified
to study the thermal decomposition of hydrocarbon fuel surrogates. Transhydrindane
(C9H16), comparable to trans-decalin ((C9H18), was selected as
a bicyclic alkane substitute for diesel or jet fuel, while methyl cyclopentane
((C6H12)), a branched monocyclic alkane, was chosen for naphtha or gasoline
in the pyrolysis experiments. A wide variety of hydrocarbons, such as alkanes,
alkenes, cycloalkanes, and aromatics, were identified through GC (gas
chromatography) analysis. The experimental results were validated against a
detailed kinetic model developed from high-level quantum chemistry and rate
calculations, which provides fundamental insights into the elementary steps
of the thermal decomposition. These studies will be further used within the
laboratory to develop surrogates for ongoing RP-1 (rocket propellant) fuel experiments
in the shock tube and the new flow reactor facility.
In conclusion, Chapter 06 summarizes the findings from the shock tube
experiments used to develop and validate theoretical kinetic models, which in
turn facilitate the interpretation of experimental observations, resulting in an
in-depth understanding of PAH chemistry in both Earth and astrophysical settings.
In addition to these chapters, the appendix contains the detailed reaction
mechanisms for the pyrolysis of both hydrindane and methylcyclopentane

