Zobrazeno 1 - 6
of 6
pro vyhledávání: '"Mahesh Ingole"'
Publikováno v:
Combustion and Flame. 209:363-375
The combustion characteristics of Ammonium Perchlorate (AP) monopropellant have been revisited. The use of silica grease to prevent heat loss from the sides of the pellet and the ignition methodology opened up new area; one of them being the low pres
Publikováno v:
Combustion and Flame. 207:356-367
This paper deals with the low pressure deflagration limit (LPDL), which is the minimum pressure below which burning of a propellant ceases without the assistance of an external energy source. The LPDL of AP monopropellant reported in literature is ar
Publikováno v:
Innovative Energetic Materials: Properties, Combustion Performance and Application ISBN: 9789811548307
The combustion characteristics of ammonium perchlorate (AP) monopropellant have been discussed. Both experimental and computational tools were utilized to explore AP combustion. Three different methods were used to determine the low-pressure deflagra
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::28394a809597e09ab29418cd561646f7
https://doi.org/10.1007/978-981-15-4831-4_9
https://doi.org/10.1007/978-981-15-4831-4_9
Autor:
Arunava Dutta, A.K. Patra, Mahesh Ingole, Moumita Dhara, P. U. Sastry, Tushar Jana, Nitai Giri
Publikováno v:
Polymer. 204:122807
This article addresses the effect of enhanced segmental mixing on various physical properties of ferrocenylsilane tethered polybutadiene based polyurethane (PU). To study this, 2-(ferrocenylpropyl) dimethylsilane (FPDS) has been grafted to the pendan
Autor:
Nitai Giri, B. Narasimha Rao, A.K. Patra, P. U. Sastry, Mahesh Ingole, Tushar Jana, Moumita Dhara
Publikováno v:
European Polymer Journal. 122:109380
Series of metal based polyurethanes (PUs) have been synthesized from hydroxyl terminated polybutadiene (HTPB) with combination of a potential energetic material, 2,4-dinitrobenzene (DNB) and burn rate (BR) enhancer, ferrocene with two objectives: (1)
This book focuses on the combustion performance and application of innovative energetic materials for solid and hybrid space rocket propulsion. It provides a comprehensive overview of advanced technologies in the field of innovative energetic materia