| 1. | The best parameters are : negtive bias voltage 200v ; deposition time 10min
Ao对kapton薄膜有较严重的侵蚀作用。 |
| 2. | Effects of electron irradiation energy on optical properties of kapton al thermal control coatings
热控涂层光学性能的影响 |
| 3. | The adhension force of kapton and protective film were characterized on scratching test equipment
利用划痕试验分析不同工艺制备的防护膜与kapton膜的结合情况。 |
| 4. | The kapton undergo dramatically degradation and the oxide coating of al or si has excellent properties for ao effects in the course of atomic oxygen beam exposures
当负偏压为200v ,镀膜时间为10min时得到的防护膜与kapton膜的结合力最好。 |
| 5. | The phases structure of the kapton film and protective film were determined by x - ray diffraction ( xrd ) and x - ray photoelectron spectroscopy ( xps )
用x射线衍射分析( xrd ) 、光电子能谱( xps )对基体薄膜及镀膜的物相成分、化学结构进行表征。 |
| 6. | Negtive bias voltage and deposition time were changed to examine their role on the property of adhension between kapton film and oxide coating of al or si
本文利用al - si合金和纯al作为靶材,通过多弧离子镀的方法在kapton膜上制备防护膜层。 |
| 7. | Then both kapton film and protective coating were exposured on the ground - based simulation facilities for ao to study the erosion behavior of kapton and protective film
然后在原子氧( atomicoxygen , ao )侵蚀地面模拟设备中对kapton薄膜以及防护膜进行原子氧侵蚀试验。 |
| 8. | A gas - jet - type vuv source that can give a spectrum in the wavelength range of 5 ~ 200nm was used in this paper to research of vuv radiation effects on upilex films which used as canopy of the space inflatable antennas and al / kapton films
利用射流式真空紫外地面模拟设备研究了5 200nm波长范围内的真空紫外辐照对al / kapton薄膜与空间充气展开天线透射面材料upilex薄膜的性能影响。 |
| 9. | Zero - expansion models satisfy the request of space structures for they can possess high dimensional stability in temperature - change fields . the surface morphology , electrical conductivity and spectral reflectivity of al / kapton films before and after space environment simulated tests were
对于al / kapton薄膜试验分别采用原子力显微镜、四探针电阻测量仪、紫外可见分光光度计测试其空间环境试验后的表面形貌、面电导率、光学反射率。 |
| 10. | Kapton is used extensively on spacecraft primarily as flexible substrates for lightweight , high - power solar arrays because of its inherent strength , temperature stability , excellent insulation properties , ultraviolet ( uv ) stability and infrared ( ir ) transparency . however , polymeric material undergoes severe degration after being exposured on atomic oxygen ( ao ) in low earth oribit ( leo )
聚合物kapton由于具有较高的比强度,优越的热稳定性、绝缘性、紫外线辐射稳定性及红外线穿透功能,是航天飞行器常用的材料,但由于空间环境中的原子氧对这种材料造成极大的损害,大大限制了这种材料在空间环境下服役时间。 |
