Heat of Explosion and Acceleration Ability of Explosive Compositions Containing Polytetrafluoroethylene

2020 ◽  
Vol 14 (1) ◽  
pp. 45-51
Author(s):  
M. N. Makhov
2012 ◽  
Vol 2012 ◽  
pp. 1-11 ◽  
Author(s):  
Ricardo Infante-Castillo ◽  
Samuel P. Hernández-Rivera

This work presents a new quantitative model to predict the heat of explosion of nitroaromatic compounds using the natural bond orbital (NBO) charge and 15N NMR chemical shifts of the nitro groups (15NNitro) as structural parameters. The values of the heat of explosion predicted for 21 nitroaromatic compounds using the model described here were compared with experimental data. The prediction ability of the model was assessed by the leave-one-out cross-validation method. The cross-validation results show that the model is significant and stable and that the predicted accuracy is within 0.146 MJ kg−1, with an overall root mean squared error of prediction (RMSEP) below 0.183 MJ kg−1. Strong correlations were observed between the heat of explosion and the charges (R2 = 0.9533) and 15N NMR chemical shifts (R2 = 0.9531) of the studied compounds. In addition, the dependence of the heat of explosion on the presence of activating or deactivating groups of nitroaromatic explosives was analyzed. All calculations, including optimizations, NBO charges, and 15NNitro NMR chemical shifts analyses, were performed using density functional theory (DFT) and a 6-311+G(2d,p) basis set. Based on these results, this practical quantitative model can be used as a tool in the design and development of highly energetic materials (HEM) based on nitroaromatic compounds.


2020 ◽  
Vol 71 (9) ◽  
pp. 87-97
Author(s):  
Titi Paraschiv ◽  
Tudor Viorel Tiganescu ◽  
George Ovidiu Iorga ◽  
Raluca Elena Ginghina ◽  
Octavian Constantin Grigoroiu

Nitrocellulose based propellants are the main materials used for ballistic and rocket applications. The chemical composition of the propellants, the loading density and propellant grain geometry are the decisive parameters that influence the performance parameters in ballistic application. In this paper the authors evaluate three models of combustion for energetic materials for the determination of heat of explosion and specific volume together with the adiabatic flame temperature. The authors select six types of propellant (two simple base propellants, two double base propellants based on nitroglycerine and two triple base propellants based on nitroguanidine) and the authors determined the heat of explosion and specific volume using a bomb calorimeter and a Julius-Peters device. The results obtained from the combustion models were compared to the experimental results and assumptions were done on the influence of pressure and temperature on the chemical composition of combustion gases produced by the confined deflagration of nitrocellulose-based propellants.


2014 ◽  
Vol 116 (14) ◽  
pp. 144906 ◽  
Author(s):  
Z. Q. Zhou ◽  
J. X. Nie ◽  
Z. C. Ou ◽  
J. F. Qin ◽  
Q. J. Jiao

1977 ◽  
Vol 28 ◽  
pp. 291-293 ◽  
Author(s):  
H.L. Girdhar ◽  
A.J. Arora

2020 ◽  
Vol 102 (4) ◽  
pp. 14-21 ◽  
Author(s):  
Jonathan A. Plucker ◽  
Carolyn M. Callahan

There is substantial evidence on the effectiveness of many forms of advanced education, especially various approaches to acceleration, ability grouping, and curricular innovations such as structured curriculum and enrichment. Nonetheless, additional research on the ways in which advanced education impacts the learning and lives of students across the variables of class, race, ethnicity, and gender is still needed, as it is for most educational interventions. Jonathan Plucker and Carolyn Callahan share the evidence base for several popular strategies and describe what evidence is still needed.


2014 ◽  
Vol 28 (10) ◽  
pp. 2738-2745 ◽  
Author(s):  
Naoki Kawamori ◽  
Robert U. Newton ◽  
Naruhiro Hori ◽  
Kazunori Nosaka

2009 ◽  
Vol 161 (2-3) ◽  
pp. 714-717 ◽  
Author(s):  
H. Muthurajan ◽  
R. Sivabalan ◽  
N. Pon Saravanan ◽  
M.B. Talawar

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