Juliano Ribeiro Aguiar Pinto

ORCID: 0000-0002-5510-0901
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About
Contact & Profiles
Research Areas
  • Polymer crystallization and properties
  • Carbon Nanotubes in Composites
  • Polymer Nanocomposites and Properties
  • Energetic Materials and Combustion
  • Rocket and propulsion systems research
  • Thermal and Kinetic Analysis
  • Chemical Thermodynamics and Molecular Structure
  • Polymer Foaming and Composites
  • Plant Surface Properties and Treatments
  • Gas Dynamics and Kinetic Theory
  • Graphite, nuclear technology, radiation studies
  • Photopolymerization techniques and applications
  • Spacecraft and Cryogenic Technologies
  • Tribology and Wear Analysis
  • Epoxy Resin Curing Processes

Instituto de Aeronáutica e Espaço
2016-2021

Instituto Tecnológico de Aeronáutica
2016-2018

Departamento de Ciência e Tecnologia
2016

Epoxy systems are widely applied as adhesives in the aerospace industry. They have excellent adhesion properties, however, being thermosetting, epoxy show fracture brittleness characteristics. Polysulfide and polymercaptans good options to increase flexibility of adhesive. Thermal analysis techniques generally used evaluate curing degree systems. In most cases, when infrared (IR) is used, it employed qualitatively. This paper presents reaction study a DGEBA prepolymer with diethylenetriamine...

10.1590/0001-3765202120200799 article EN cc-by Anais da Academia Brasileira de Ciências 2021-01-01

Insulations for rocket motors such as Flexible Thermal Protections (FTPs) and Rigid Protection (RTPs) act thermal barriers against the hyperthermal environment from solid propellant combustion. FTPs present dual function: to extend RTPs performance, attenuate contraction. used in Brazilian Space Program have asbestos their composition since 70´s; however, they are hazardous human health. In this context, a mixture of Expanded Perlite (PExp) Cork Powder (CP) was investigated replacement...

10.1590/0001-3765201820170964 article EN cc-by Anais da Academia Brasileira de Ciências 2018-09-01

Thermal protection systems (TPS) are components designed to protect the internal and external areas of a rocket motor from high temperatures. There has been studies in Brazil resin-based polybutadiene hydroxylated (HTPB) loaded with asbestos since 1970s. Nevertheless, banned several countries because it is severely harmful human health. In this context, development free flexible thermal (FTP) extremely important. This study evaluates use Expanded Perlite (PExp) as an substitute. Lower...

10.1590/1980-5373-mr-2017-0856 article EN cc-by Materials Research 2018-08-18
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