kapton 中文意思是什麼

kapton 解釋
聚醚亞胺
  1. The adhension force of kapton and protective film were characterized on scratching test equipment

    利用劃痕試驗分析不同工藝制備的防護膜與kapton膜的結合情況。
  2. 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由於具有較高的比強度，優越的熱穩定性、絕緣性、紫外線輻射穩定性及紅外線穿透功能，是航天飛行器常用的材料，但由於空間環境中的原子氧對這種材料造成極大的損害，大大限制了這種材料在空間環境下服役時間。
  3. 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

    當負偏壓為200v ，鍍膜時間為10min時得到的防護膜與kapton膜的結合力最好。
  4. 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射線衍射分析（ xrd ） 、光電子能譜（ xps ）對基體薄膜及鍍膜的物相成分、化學結構進行表徵。
  5. 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擬設備研究了5 200nm波長范圍內的真空紫外輻照對al / kapton薄膜與空間充氣展開天線透射面材料upilex薄膜的性能影響。
  6. In this paper, the vacuum thermo - cycling effects and vacuum ultraviolet effects on space inflatable structural materials were analyzed based on a thorough survey over the studies done through flight tests, ground simulation experiments and theoretical research. the main contents of this thesis are as follows : the performance damage effects of thermo - cycling on space inflatable structural fabric carbon fiber reinforced epoxy laminates ( cf / ep ), aluminized kapton ( al / kapton ) films which used as reflector of space inflatable antenna were investigated by a temperature range of - 120 120 with the vacuum degree 10 - 5 pa which conducted with space environment ground - based simulation facility

    本文在對國內外飛行試驗、地面模擬試驗以及理論研究等所取得的成果調研的基礎上，針對空間充氣結構材料進行地面模擬真空熱循環與真空紫外輻照的研究工作:利用真空熱循環地面模擬試驗機研究了真空環境（ 10 - 5pa ）中- 120 120的熱循環條件下空間充氣支撐結構織物碳纖維增強環氧樹脂（ cf / ep ）層合材料、空間充氣展開天線反射面鍍鋁聚酰亞胺（ al / kapton ）薄膜的空間環境效應。
  7. 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

    對于al / kapton薄膜試驗分別採用原子力顯微鏡、四探針電阻測量儀、紫外可見分光光度計測試其空間環境試驗后的表面形貌、面電導率、光學反射率。
  8. 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合金和純al作為靶材，通過多弧離子鍍的方法在kapton膜上制備防護膜層。
  9. 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

    然後在原子氧（ atomicoxygen ， ao ）侵蝕地面模擬設備中對kapton薄膜以及防護膜進行原子氧侵蝕試驗。
  10. Effects of electron irradiation energy on optical properties of kapton al thermal control coatings

    熱控塗層光學性能的影響
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