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Haridwar Singh

Researcher at High Energy Materials Research Laboratory

Publications -  67
Citations -  1375

Haridwar Singh is an academic researcher from High Energy Materials Research Laboratory. The author has contributed to research in topics: Propellant & Ammonium perchlorate. The author has an hindex of 18, co-authored 67 publications receiving 1209 citations. Previous affiliations of Haridwar Singh include University of Hyderabad & Defence Institute of Advanced Technology.

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Hexanitrohexaazaisowurtzitane (CL-20) and CL-20-based formulations (review)

TL;DR: A review of the research and development work on CL-20, the most powerful high-energy material of today, as well as CL20-based formulations is presented in this article.
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Important aspects of behaviour of organic energetic compounds: a review.

TL;DR: In this paper, the importance of a prediction tool increases with greater relevance for synthesis, performance and vulnerability predictions, and some important aspects of performance behavior and their theoretical calculations, which are indispensable in recognizing energetic molecules of interest, are described.
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Studies on cl-20: the most powerful high energy material

TL;DR: In this article, the authors made an attempt to explain the mechanism of decomposition of CL-20 on the basis of the data obtained by the authors and findings of other researchers, and the activation energy values obtained during this work by adopting various approaches are close to the values reported for NNO2 bond cleavage suggesting that it is global rate determining process rather than the collapse of cage structure.
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Energetic plasticizers for gun & rocket propellants

TL;DR: In this paper, the recent advances in the field of energetic plasticizers with special reference to their applications in gun and rocket propellants are discussed, as well as future scope for R&D work in this area.
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Glycidyl azide polymer (GAP) − An energetic component of advanced solid rocket propellants − A review

TL;DR: In this paper, the physicochemical, thermal, mechanical and ballistic properties of GAP and GAP-based solid propellants are reviewed and compared with those of traditional solid propellant compositions.