紀要論文

Measuring carbon fiber aging on orbit

eng

21888507

https://doi.org/10.15002/00010555

法政大学情報科学部・理工学部・生命科学部

50

01

06

2014-04

Version of Record

This paper describes the outcome of internship at the faculty of science and engineering, Hosei University in summer 2014. The goal of the project is to design a measuring system of aging properties of a carbon fiber reinforced composite in space. The project is a part of the nano-satellite project at Czech Technical University in Prague, scheduled to be launched in 2016. The measurement environment In space is different from the standard measurements performed on the ground in laboratory. The system design specification has a large constraint in size, weight and power consumption by the limit of space probes. To meet these requirement, the basic measuring system of the mechanical damping characteristics of the carbon fiber composite is designed in this internship project. A damping oscillator to simulate the response of the target material has been assembled and measuring parameters arc optimized. The optimized algorithm has been implemented in the chip to be launched on the space orbit.

Article

AA12565158