Zobrazeno 1 - 7
of 7
pro vyhledávání: '"Márcio Yuji Nagamachi"'
Autor:
José Irineu Sampaio de Oliveira, Márcio Yuji Nagamachi, Milton Faria Diniz, Elizabeth da Costa Mattos, Rita de Cássia Lazzarini Dutra
Publikováno v:
Journal of Aerospace Technology and Management, Vol 3, Iss 3, Pp 269-278 (2011)
Over the last two decades, many routes have been proposed to synthesize ammonium dinitramide (ADN). However, most of them lie in routes in which reactants are too expensive for large-scale production. In this sense, the use of ordinary reactants is o
Externí odkaz:
https://doaj.org/article/e74d7cb2ad374a969daf8b63139e3b03
Autor:
José Irineu Sampaio de Oliveira, Márcio Yuji Nagamachi, Milton Faria Diniz, Elizabeth da Costa Mattos, Rita Lazzarini Dutra
Publikováno v:
Journal of Aerospace Technology and Management, Vol 3, Iss 3 (2012)
Over the last two decades, many routes have been proposed to synthesize ammonium dinitramide (ADN). However, most of them lie in routes in which reactants are too expensive for large-scale production. In this sense, the use of ordinary reactants is o
Externí odkaz:
https://doaj.org/article/96fc8096b5a7431cbc7b308e353d53ef
Autor:
José Irineu Sampaio de Oliveira, Márcio Yuji Nagamachi, Rita de Cássia Lazzarini Dutra, Milton Faria Diniz, Elizabeth da Costa Mattos
Publikováno v:
Journal of Aerospace Technology and Management. 3:269-278
Over the last two decades, many routes have been proposed to synthesize ammonium dinitramide (ADN). However, most of them lie in routes in which reactants are too expensive for large-scale production. In this sense, the use of ordinary reactants is o
Autor:
Márcio Yuji Nagamachi, Rita de Cássia Lazzarini Dutra, Aparecida M. Kawamoto, José Irineu Sampaio de Oliveira
Publikováno v:
Journal of Aerospace Technology and Management, Vol 1, Iss 2, Pp 153-160 (2009)
Journal of Aerospace Technology and Management, Volume: 1, Issue: 2, Pages: 153-160, Published: DEC 2009
Journal of Aerospace Technology and Management v.1 n.2 2009
Journal of Aerospace Technology and Management
Departamento de Ciência e Tecnologia Aeroespacial (DCTA)
instacron:DCTA
Journal of Aerospace Technology and Management, Volume: 1, Issue: 2, Pages: 153-160, Published: DEC 2009
Journal of Aerospace Technology and Management v.1 n.2 2009
Journal of Aerospace Technology and Management
Departamento de Ciência e Tecnologia Aeroespacial (DCTA)
instacron:DCTA
The search for a smokeless propellant has encouraged scientists and engineers to look for a chlorine-free oxidizer as a substitute for AP (ammonium perchlorate). Endeavors seemed to come to an end when ADN (ammonium dinitramide) appeared in the West
Autor:
Paula Cristina Gomes Fernandes, Jessica Santos Gomes, Elizabete Yoshie Kawachi, Marcio Yuji Nagamachi, Luiz Fernando de Araujo F Ferrão, Kamila Pereira Cardoso
Publikováno v:
Journal of Aerospace Technology and Management, Vol 11, Iss 1 (2020)
Paraffin-based hybrid propellants have been developed due to their high burning rate. However, they have some disadvantages such as inadequate mechanical properties and unstable burning. In this work, paraffin fuel grains with carbon black were evalu
Externí odkaz:
https://doaj.org/article/55ccdb2ee4844f1fb99f4a06a8fd2737
Autor:
Jessica de Oliveira Silva, Josiane Ribeiro Campos Silva, Lucas Barros de Oliveira, Marcio Yuji Nagamachi, Luiz Fernando de Araujo Ferrão
Publikováno v:
Journal of Aerospace Technology and Management, Vol 11, Iss 1 (2020)
In composite solid propellants, the oxidizer in the form of particles is embedded in a polymeric matrix. In general, these oxidizers consist in inorganic salts that are hygroscopic, chemically incompatible or sensitive to friction or impact, so that
Externí odkaz:
https://doaj.org/article/9191101792164ea6b015d539d4c750f9
Autor:
Lia Junqueira Pimont, Paula Cristina Gomes Fernandes, Luiz Fernando de Araujo Ferrão, Marcio Yuji Nagamachi, Kamila Pereira Cardoso
Publikováno v:
Journal of Aerospace Technology and Management, Vol 11, Iss 1 (2020)
A gas generating propellants are used as initiators of liquid rocket propellants turbopumps and have as desired characteristic a high-volume production of low-temperature gas. In this context, some formulations of composite propellant containing poly
Externí odkaz:
https://doaj.org/article/a449c4948d94406eab7c898201bfbe6c