Vol. 5 No. 3 (2013): Jul./Sep., 2013

Editorial

Spin-off Companies: A Great Challenge for the Brazilian Space Program

Marcia Mantelli

265-266
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Review Articles

An Overview of the Technological Progress in Propellants Using Hydroxyl-Terminated Polybutadiene as Binder During 2002–2012

Gilson da Silva, Simone Carvalho Rufino, Koshun Iha

267-278
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Original Papers

Experimental Study of Polyurethane-Based Fuels with Addition of Paraffin and Aluminum for Hybrid Rocket Motors

Susane Ribeiro Gomes, Leopoldo Rocco Junior, José Atílio Fritz Fidel Rocco, Koshun Iha

279-286
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Combustion Modeling of Aluminum Incorporated in Low-Explosive Formulations such as Solid Propellants

Rene F. Boschi Gonçalves, Koshun Iha, José Atílio Fritz F. Rocco

287-292
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Kick Solid Rocket Motor Multidisciplinary Design Optimization Using Genetic Algorithm

Fredy Marcell Villanueva, He Linshu, Xu Dajun

293-304
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Simulations of the Atmospheric Boundary Layer in a Wind Tunnel with Short Test Section

Luciana Bassi Marinho Pires, Igor Braga de Paula, Gilberto Fisch, Ralf Gielow, Roberto da Mota Girardi

305-314
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Verification of Response of Neutron Monitor for In-Flight Neutron Dosimetry

Claudio Antonio Federico, Odair Lelis Gonçales, Evaldo Simões da Fonseca, Karla Cristina de Souza Patrão, Marlon Antonio Pereira, Linda Viola Ehlin Caldas

315-322
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Compiler Optimizations Impact the Reliability of the Control-Flow of Radiation-Hardened Software

Ronaldo Rodrigues Ferreira, Rafael Baldiati Parizi, Luigi Carro, Álvaro Freitas Moreira

323-334
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Analysis of Total Ionizing Dose Effects on 0.13µm Technology-Temperature-Compensated Voltage References

Thiago Hanna Both, Dalton Colombo, Ricardo Vanni Dallasen, Gilson Inácio Wirth

335-340
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Nonlinear Characteristics of Revolute Joints with Clearance

Liu Rong-qiang, Jing Zhang, Guo Hong-wei, Deng Zong-quan

341-348
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Optimal Design of a High-altitude Solar-Powered Unmanned Airplane

Bento Silva de Mattos, Ney Rafael Secco, Eduardo Francisco Salles

349-361
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Editorial

Spin-off Companies: A Great Challenge for the Brazilian Space Program

Review Articles

An Overview of the Technological Progress in Propellants Using Hydroxyl-Terminated Polybutadiene as Binder During 2002–2012

Original Papers

Experimental Study of Polyurethane-Based Fuels with Addition of Paraffin and Aluminum for Hybrid Rocket Motors

Combustion Modeling of Aluminum Incorporated in Low-Explosive Formulations such as Solid Propellants

Kick Solid Rocket Motor Multidisciplinary Design Optimization Using Genetic Algorithm

Simulations of the Atmospheric Boundary Layer in a Wind Tunnel with Short Test Section

Verification of Response of Neutron Monitor for In-Flight Neutron Dosimetry

Compiler Optimizations Impact the Reliability of the Control-Flow of Radiation-Hardened Software

Analysis of Total Ionizing Dose Effects on 0.13µm Technology-Temperature-Compensated Voltage References

Nonlinear Characteristics of Revolute Joints with Clearance

Optimal Design of a High-altitude Solar-Powered Unmanned Airplane

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