“…Air-breathing propulsion systems rely on the combustion of hydrocarbon fuels such as of Jet Propellant-10 (JP-10). , The exo -tetrahydrodicyclopentadiene molecule (C 10 H 16 ; Scheme ) represents the major component of JP-10 and is defined by a high volumetric energy (39.6 kJ cm –3 ) due to three five-membered ring moieties incorporated into a single molecule along with the inherent ring strain energy. This makes JP-10 not only an attractive fuel for missiles, pulse-detonation engines, and ramjets ,, but also interesting for the physical (organic) chemistry, combustion, and theoretical chemistry communities to explore its decomposition and oxidation experimentally, theoretically, and in combustion models. − Exploiting shock tubes, flow tubes, ,− and high-temperature chemical reactors, ,, a detailed understanding of the decomposition of pure JP-10 is beginning to emerge. The unimolecular decomposition (“pyrolysis”) of JP-10 leads to smaller hydrocarbon molecules and reactive transient species, among them aliphatic radicals, resonantly stabilized free radicals (RSFRs), and aromatic radicals (ARs), , which initiate the complex chemistry in the oxidation of JP-10 based jet fuel.…”