Informacja

Drogi użytkowniku, aplikacja do prawidłowego działania wymaga obsługi JavaScript. Proszę włącz obsługę JavaScript w Twojej przeglądarce.

Wyszukujesz frazę "Sadavarte, V. S." wg kryterium: Autor


Wyświetlanie 1-3 z 3
Tytuł:
Studies on Sensitivity of Nitrate Ester Plasticized Hydroxyl Terminated Prepolymer Based Energetic Solid Rocket Propellants
Autorzy:
Bhowmik, D.
Sadavarte, V. S.
Charbhe, V. D.
Pande, S. M.
Powiązania:
https://bibliotekanauki.pl/articles/358663.pdf
Data publikacji:
2017
Wydawca:
Sieć Badawcza Łukasiewicz - Instytut Przemysłu Organicznego
Tematy:
sensitivity
impact
friction
card gap test
DDT test
SLSG test
Opis:
The sensitivities of energetic materials as well as advanced energetic solid propellants are invariably associated with the nature of the stimuli that are responsible for the initiation of their decomposition. Hence it is important to study the chemical processes involved with these decompositions. While assessing the potential application of new propellant formulations containing energetic materials, it is important to assess their sensitivity to the hazards involved during their handling, transport, storage and use. This paper reports the results of impact, friction, heat, spark and shock sensitivities of advanced high energy solid rocket propellant formulations based on nitrate ester plasticized, hydroxyl terminated prepolymer (SPB-255) as an energetic binder loaded with solid ingredients like ammonium perchlorate (AP), aluminium (Al) and cyclotetramethylenetetranitramine (HMX). The results of the small card gap test showed that they are more sensitive than a composite modified double base (CMDB) propellant, which in turn is more sensitive than double base (DB) as well as composite propellants. Deflagration to detonation transition (DDT) tests carried out for the advanced energetic propellant did not show any detonation phenomena. Trinitrotoluene (TNT) equivalence and super large scale gap (SLSG) tests have been carried out for the determination of hazard classification of the energetic solid rocket propellant. The requirements to achieve both higher performance in terms of improved energy (i.e., specific impulse, Isp) and reduced sensitivity for the same propellant composition are contradictory; one should be sacrificed for the other, within manageable limits.
Źródło:
Central European Journal of Energetic Materials; 2017, 14, 3; 605-620
1733-7178
Pojawia się w:
Central European Journal of Energetic Materials
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
An Energetic Binder for the Formulation of Advanced Solid Rocket Propellants
Autorzy:
Bhowmik, D.
Sadavarte, V. S.
Pande, S. M.
Saraswat, B. S.
Powiązania:
https://bibliotekanauki.pl/articles/358431.pdf
Data publikacji:
2015
Wydawca:
Sieć Badawcza Łukasiewicz - Instytut Przemysłu Organicznego
Tematy:
BTTN
polyol
low temperature strain capability
glass transition temperature
gel time
Opis:
Many promising elastomers and energetic binders are reported in the literature for their probable application in propellant formulations. However, their application in actual systems is still restricted due to many inherent limitations. Therefore, an attempt has been made to study the performance of an advanced energetic solid propellant based on an energetic binder comprising a polyol with high hydroxyl functionality plasticized with 1,2,4-butanetriol trinitrate (BTTN). In order to examine the physico-chemical properties of the BTTN/Polyol binder system, the polyol and a series of binders have been formulated and cured with different di-isocyanates viz. TDI, IPDI and H12MDI, and the cured binder sheets were evaluated for their mechanical properties, decomposition temperatures and glass transition temperatures (Tg). The pot life of a representative binder system with various di-isocyanates has also been determined using a gelation timer apparatus. The overall result of this study establishes that the energetic binder system under study has potential applications in the formulation and processing of advanced energetic solid propellant compositions for case bonded rocket motors, offering higher density, higher energy and better low temperature strain capability as compared to conventional HTPB-based composite propellants.
Źródło:
Central European Journal of Energetic Materials; 2015, 12, 1; 145-158
1733-7178
Pojawia się w:
Central European Journal of Energetic Materials
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Studies on the Effect of Nitrate Esters on the Properties of Advanced Energetic Propellants
Autorzy:
Kumar, Amit
Chavan, Prakash V
Sadavarte, Vaibhav S
Bhowmik, Debdas
Mada, S.S.N.M. Santosh
Pande, Shrikant M.
Powiązania:
https://bibliotekanauki.pl/articles/1062883.pdf
Data publikacji:
2020
Wydawca:
Sieć Badawcza Łukasiewicz - Instytut Przemysłu Organicznego
Tematy:
nitroglycerine
NG
butanetriol trinitrate
BTTN
strain capability
thermal decomposition
Opis:
Propulsion designers all over the world are exploring the possibility of achieving higher performance by enhancing the energy of solid propellants. This can be achieved by replacing non-energetic ingredients with energetic ones or by replacing low density ingredients, particularly binders, with higher density ones, without affecting the processibility and ageing characteristics. The same has been attempted by using nitroglycerine (NG) and butanetriol trinitrate (BTTN) as plasticizers in propellant compositions. In the present study, NG and BTTN have been used in different plasticizer to polymer ratios (Pl/Po) and various parameters of each composition have been theoretically predicted. Three propellant compositions plasticized with NG, BTTN and a 1:1 combination of NG and BTTN, have been processed and analyzed for targeted properties. From the theoretical data, it was observed that there is a negligible increase in density impulse beyond a Pl/Po ratio of 2, apart from the higher density and calorimetric values of the NG-plasticized propellant; these plasticizers have a significant effect on the ballistic and mechanical properties. Another observation was that the elongation of BTTN and NG/BTTN (1:1) plasticized propellants is significantly higher at a low crosshead rate than NG-plasticized propellant, implying that the two former propellants have higher strain capabilities at low temperatures and can be used for missiles having long term low temperature storage requirements. Thermal decomposition studies have been carried out by DSC, and for each composition 5 distinct peaks were observed.
Źródło:
Central European Journal of Energetic Materials; 2020, 17, 3; 384-407
1733-7178
Pojawia się w:
Central European Journal of Energetic Materials
Dostawca treści:
Biblioteka Nauki
Artykuł
    Wyświetlanie 1-3 z 3

    Ta witryna wykorzystuje pliki cookies do przechowywania informacji na Twoim komputerze. Pliki cookies stosujemy w celu świadczenia usług na najwyższym poziomie, w tym w sposób dostosowany do indywidualnych potrzeb. Korzystanie z witryny bez zmiany ustawień dotyczących cookies oznacza, że będą one zamieszczane w Twoim komputerze. W każdym momencie możesz dokonać zmiany ustawień dotyczących cookies