Evaluation of effective emissivity of new thermal insulation using polyimide foam for spacecraft

Ryuichi Takagi, Sumitaka Tachikawa, Yuji Nagasaka

研究成果: Conference contribution

1 被引用数 (Scopus)


Conventionally, multilayer insulation (MLI) has been used for spacecraft, and known for high performance thermal insulation. MLI blanket is composed of multiple layers of low cmittance films with spacers. The layers are stacked and sewn together at the edge, and attached to the spacecraft using Velcro on one side of MLI blanket. Though, heat losses through Seam and Velcro make the performance of MLI degraded. Saving heater power is the key factor for deep space missions or lunar exploratory missions. Therefore, local thermal insulation performance degradation is unacceptable. In order to respond to this situation, we focus on polyimide foam (PF) and propose polyimide foam multilayer insulation (PF-MLI), which shows superior performance compared with conventional MLI blanket. Thermal conductivity of PF measured and estimated in this study change with density, and local minimum value, are ascertained from both measurement and estimation. Based on these results, the optimum configuration (layers, density, etc.) of PF-MLI is determined. PF-MLI is composed of aluminized films and PF between films. Two different types of PF are used for PF-MLI and compared with Standard MLI Blanket in terms of effective emissivity and weight. Type BF301 (6~8 kg/m3) with aluminized films and Type BP 101 (29-33 kg/m3) with aluminized films are the measurement samples as PF-MLI, and two different layer numbers are fabricated in each sample. Guarded hot plate method, which is useful heat flux measurement method with reducing heat loss, is applied to measure effective emissivity in a vacuum steady-state condition. Effective emissivity is calculated from the higher temperature, colder temperature of the sample, and heat flux thorough the sample from Stephan Boltzmann law in a steady-state. As a result, effective emissivity of PF-MLI is lower than that of Standard MLI in higher temperature range from 260K to 340K, and it can be concluded that especially PF-MLI using BF301 (7.2 kg/m3) is the optimum thermal insulation from the standpoint of lighter weight and higher performance. In addition, seam effect on degrading the performance is not serious and high performance is expected compared with conventional MLI, whose heat loss is critical to degrading the performance.

ホスト出版物のタイトル63rd International Astronautical Congress 2012, IAC 2012
出版ステータスPublished - 2012 12月 1
イベント63rd International Astronautical Congress 2012, IAC 2012 - Naples, Italy
継続期間: 2012 10月 12012 10月 5


名前Proceedings of the International Astronautical Congress, IAC


Other63rd International Astronautical Congress 2012, IAC 2012

ASJC Scopus subject areas

  • 航空宇宙工学
  • 天文学と天体物理学
  • 宇宙惑星科学


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