Network


Latest external collaboration on country level. Dive into details by clicking on the dots.

Hotspot


Dive into the research topics where R. Rajeev is active.

Publication


Featured researches published by R. Rajeev.


Thermochimica Acta | 1995

Thermal decomposition studies. Part 19. Kinetics and mechanism of thermal decomposition of copper ammonium chromate precursor to copper chromite catalyst and correlation of surface parameters of the catalyst with propellant burning rate

R. Rajeev; K.A. Devi; Annamma Abraham; K. Krishnan; T.E. Krishnan; K.N. Ninan; C.G.R. Nair

Abstract The thermal decomposition of copper ammonium chromate (CAC), which is a precursor of copper chromite (CC) catalyst (used as a ballistic modifier in solid propellants), has been thoroughly studied. The DTG curves show that there are three main peaks at about 286, 440 and 740°C, whereas DTA gives peaks at 254 (endo), 278 (exo), 408 (exo) and 699°C (endo). The kinetic parameters for the prominent and clear-cut first stage in TG (DTG peak at 286°C) are E = 236 kJ mol−1, A = 1.51 × 1021 s−1, and Δ = 136 J K−1 mol−1. The mechanism of this decomposition reaction is identified as a phase boundary reaction with spherical symmetry, as per the equation g(α) = 1 − (1 − α) 1 3 . The surface parameters of the CC samples obtained by calcination of CAC, at different temperature regimes compatible with TG data, have been determined. The surface area of the CC decreases when the calcination temperature increases. The surface area also decreases when CC samples are washed with acetic acid. X-ray diffraction (XRD) patterns of CC samples obtained from higher temperature calcinations of CAC differ from those obtained at lower temperatures. The propellant burning rate is enhanced by the addition of CC and increases when the Lewis acid amounts of the catalyst sample increase. These correlations have been established for the first time for CC catalysts used in propellant technology.


Journal of Thermal Analysis and Calorimetry | 2016

TG–MS study on the kinetics and mechanism of thermal decomposition of copper ethylamine chromate, a new precursor for copper chromite catalyst

Sanoop Paulose; Deepthi Thomas; T. Jayalatha; R. Rajeev; Benny K. George

Abstract Copper chromite is a well-known burn rate modifier for the combustion of composite solid propellants. In this study, basic copper ethylamine chromate (CEC), a new precursor for copper chromite catalyst, was synthesized by precipitation method. The thermal decomposition of the precursor was followed by thermogravimetry–mass spectroscopy (TG–MS) and X-ray diffraction techniques and compared with that of copper ammonium chromate, a conventional precursor for copper chromite catalyst. TG–MS analysis for the decomposition of CEC revealed that the decomposition starts with the liberation of ethylamine. The change in enthalpy for the decomposition reaction of copper ethylamine chromate was higher than that of copper ammonium chromate due to the oxidation of ethyl group. The reducing atmosphere created by the presence of carbon during the decomposition of CEC produced a mixture of Cu, CuCr2O4, CuCrO2 and CuO, while the oxidizing atmosphere of copper ammonium chromate produced a mixture of CuCr2O4 and CuO. Mechanistic study based on Criado and Coats–Redfern methods showed that CEC follows random nucleation (F1) mechanism as the rate-determining step for the thermal decomposition process.


New Journal of Chemistry | 2017

New insights into the spectral, thermal and morphological analysis of time dependent structural changes during open end functionalization of single walled carbon nanotubes

Rinu Elizabeth Roy; Bhuvaneswari Soundiraraju; Deepthi Thomas; Nisha Balachandran; Chithra Ambika; R. Rajeev

Even though several authors have investigated the chemical derivation of single walled carbon nanotubes (SWCNTs) through their treatment with concentrated nitric acid (conc. HNO3), this paper reports hitherto unaccounted for insights in this field of study that can be achieved through a spectral, thermal and morphological evaluation of SWCNTs, functionalized at a fixed temperature for different time intervals. In this study, multiple techniques were employed to systematically evaluate the structural changes on SWCNTs with refluxing time. Furthermore, the nanotubes, specifically functionalized for different extents of time, were characterized using a combination of analytical techniques including Raman spectroscopy, thermogravimetry-mass spectroscopy (TG-MS), X-ray photoelectron spectroscopy (XPS) and ultra violet near infrared spectroscopy (UV-Vis-NIR). To arrive at an optimum reflux point, an analysis of the changes in Radial Breathing Mode (RBM), D-band & G-band of Raman spectra, TG-MS profile and Zeta potential measurements was carried out. TG-MS (of the evolved carbon dioxide) and XPS were employed, respectively, to quantify the acid groups in the functionalised SWCNTs (F-SWCNTs) and the type of functional groups attached onto the SWCNTs. While the electronic nature of the SWCNTs was analysed through the line-shape of the G-band, the 2D band of the Raman spectra and the UV-Vis-NIR spectra, their morphological characterisation was done using a high resolution transmission electron microscope (HRTEM). Exploiting the advantages of each characterization techniques, the reflux time for the effective functionalization of SWCNTs, without any compromise of their quality, was converged down to 4 h. This paper proposes a new mechanism to account for the multistage oxidation with the extension of reflux time and explain the type of functional groups attached onto the surface of SWCNTs as functionalization proceeds with time. It is also claimed that the changes in the relative concentration of functionalized groups on the SWCNT surface are directly proportional to the increase in the extent of functionalization. Significantly, this paper reports that the introduction of any desired ratio of functional groups on the surface of carbon nanotubes can be achieved by tuning the extent of functionalization.


Propellants, Explosives, Pyrotechnics | 1996

Thermoanalytical Investigations on the Effect of Atmospheric Oxygen on HTPB resin

K. N. Ninan; K. Krishnan; R. Rajeev; G. Viswanathan


Thermochimica Acta | 2015

Synthesis and characterization of a novel copper chromite catalyst for the thermal decomposition of ammonium perchlorate

A.P. Sanoop; R. Rajeev; Benny K. George


Process Safety and Environmental Protection | 2017

Removal of perchlorate from drinking water using granular activated carbon modified by acidic functional group: Adsorption kinetics and equilibrium studies

G Rekha Krishnan; R. Radhika; T. Jayalatha; Salu Jacob; R. Rajeev; Benny K. George; B.R. Anjali


Journal of Thermal Analysis and Calorimetry | 2017

Non-isothermal cure and decomposition kinetics of epoxy–imidazole systems

K. Leena; P. B. Soumyamol; Monisha Baby; S. Suraj; R. Rajeev; Dhanya S. Mohan


Polymer Degradation and Stability | 2018

Inherently flame retardant vinyl bearing hyperbranched polysiloxanes having improved thermal stability-Ceramization and analysis of associated thermal properties

K. Indulekha; Deepthi Thomas; N. Supriya; R. Rajeev; Dona Mathew; K. N. Ninan; C. Gouri


Ceramics International | 2018

Growth of SiOC/SiC nanostructures from cured polysiloxane-silica composite

K. Indulekha; Deepthi Thomas; R. Rajeev; K. N. Ninan; C. Gouri


Ceramics International | 2018

Cured polysiloxane-boron nitride composite as novel precursor for SiBCN nanostructures

K. Indulekha; R. Rajeev; K. N. Ninan; C. Gouri

Collaboration


Dive into the R. Rajeev's collaboration.

Top Co-Authors

Avatar

K. N. Ninan

Vikram Sarabhai Space Centre

View shared research outputs
Top Co-Authors

Avatar

C. Gouri

Vikram Sarabhai Space Centre

View shared research outputs
Top Co-Authors

Avatar

Deepthi Thomas

Vikram Sarabhai Space Centre

View shared research outputs
Top Co-Authors

Avatar

K. Indulekha

Vikram Sarabhai Space Centre

View shared research outputs
Top Co-Authors

Avatar

Benny K. George

Vikram Sarabhai Space Centre

View shared research outputs
Top Co-Authors

Avatar

T. Jayalatha

Vikram Sarabhai Space Centre

View shared research outputs
Top Co-Authors

Avatar

Dona Mathew

Vikram Sarabhai Space Centre

View shared research outputs
Top Co-Authors

Avatar

G Rekha Krishnan

Vikram Sarabhai Space Centre

View shared research outputs
Top Co-Authors

Avatar

K. Krishnan

Vikram Sarabhai Space Centre

View shared research outputs
Top Co-Authors

Avatar

R. Radhika

Vikram Sarabhai Space Centre

View shared research outputs
Researchain Logo
Decentralizing Knowledge