Synthesis, Characterization and Energetic Properties of Hydroxymethyl‐Bishomocubanone Derivatives

Author:

Lal Sohan1,Rao Cheekatla Subba1,Suresh Alati1,Ayyagari Narasimham1,Mallick Lovely2,Pallikonda Gangaram1,Desai Poonam1,Ahirwar Parmanand2,Chowdhury Arindrajit2,Kumbhakarna Neeraj2,Namboothiri Irishi N. N.1ORCID

Affiliation:

1. Department of Chemistry Indian Institute of Technology Bombay Mumbai 400076 India

2. Department of Mechanical Engineering Indian Institute of Technology Bombay Mumbai 400076 India

Abstract

AbstractThe present work reports synthesis, characterization and theoretical insights on novel hydroxymethyl‐bishomocubanone derivatives. Twelve new bishomocubanes (BHCs) were synthesized and fully characterized by various spectroscopic techniques and single crystal X‐ray analysis. The densities of the title compounds were in the range of 1.30–1.59 g/cm3. Density‐functional theory (DFT) based calculations at B3LYP/6‐311++G(d,p) level of theory were performed on ten selected BHC based cage compounds. Propulsive and ballistic properties of newly synthesized hydroxymethyl‐bishomocubanone derivatives in solid and liquid propulsion systems were calculated, and the results suggested that these compounds are superior to conventional fuel RP1 and binder HTPB. The detonation parameters revealed that these compounds are not explosive in nature and safe to use as solid propellants. Furthermore, kinetic and thermal stabilities of the title compounds were determined by HOMO‐LUMO energy gap, ESP maps, impact sensitivity (h50) and bond dissociation energies (BDEs) followed by thermogravimetric analysis (TGA) and differential thermal analysis (DTA). Three compounds, a dinitroazide (Isp,vac=310.98 s), a dinitrate (Isp,vac=309.51 s), and a dinitronitrate (Isp,vac=309.20s) were found to be excellent candidates for volume limited applications.

Funder

Indian Space Research Organisation

Publisher

Wiley

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