Minton Timothy K, Schwartzentruber Thomas E, Xu Chenbiao
Smead Department of Aerospace Engineering Sciences, University of Colorado, Boulder, Colorado 80303, United States.
Department of Aerospace Engineering and Mechanics, University of Minnesota, Minneapolis, Minnesota 55455, United States.
ACS Appl Mater Interfaces. 2021 Nov 3;13(43):51673-51684. doi: 10.1021/acsami.1c14196. Epub 2021 Oct 21.
The environment encountered by space vehicles in very low Earth orbit (VLEO, 180-350 km altitude) contains predominantly atomic oxygen (AO) and molecular nitrogen (N), which collide with ram surfaces at relative velocities of ∼7.5 km s. Structural, thermal-control, and coating materials containing organic polymers are particularly susceptible to AO attack at these high velocities, resulting in erosion, roughening, and degradation of function. Copolymerization or blending of a polymer with polyhedral oligomeric silsesquioxane (POSS) yields a material that can resist AO attack through the formation of a passivating silicon-oxide layer. Still, these hybrid organic/inorganic polymers become rough through AO reactions as the passivating layer is forming. Surface roughness may enhance satellite drag because it promotes energy transfer and scattering angle randomization during gas-surface collisions. As potential low-drag and AO-resistant materials, we have investigated POSS-containing films of clear and Kapton-like polyimides that have an atomically smooth AO-resistant coating of AlO that is grown by atomic layer deposition (ALD). Coated and uncoated films were exposed to hyperthermal molecular beams containing atomic and molecular oxygen to investigate their AO resistance, and molecular beam-surface scattering studies were conducted to characterize the gas-surface scattering dynamics on pristine and AO-exposed surfaces to inform drag predictions. The AO erosion yield of AlO ALD-coated films is essentially zero. Simulations of drag on a representative satellite structure that are based on the observed scattering dynamics suggest that the use of AlO ALD-coated POSS-polyimides on external satellite surfaces have the potential to reduce drag to less than half of that predicted for diffuse scattering surfaces. These smooth and AO-resistant polymer films thus show promise for use in an extreme oxidizing and high-drag environment in the VLEO.
航天器在近地极轨道(VLEO,海拔180 - 350千米)所遇到的环境中主要包含原子氧(AO)和分子氮(N₂),它们以约7.5千米/秒的相对速度与冲压表面碰撞。含有有机聚合物的结构材料、热控材料和涂层材料在这些高速情况下特别容易受到AO的攻击,从而导致侵蚀、表面粗糙化和功能退化。将聚合物与多面体低聚倍半硅氧烷(POSS)进行共聚或共混会产生一种材料,该材料可通过形成钝化氧化硅层来抵抗AO攻击。然而,在钝化层形成过程中,这些有机/无机杂化聚合物会因AO反应而变得粗糙。表面粗糙度可能会增加卫星的阻力,因为它会促进气体 - 表面碰撞过程中的能量转移和散射角随机化。作为潜在的低阻力和抗AO材料,我们研究了含有POSS的透明聚酰亚胺薄膜以及类似Kapton的聚酰亚胺薄膜,这些薄膜具有通过原子层沉积(ALD)生长的原子级光滑的抗AO涂层AlOₓ。对涂覆和未涂覆的薄膜进行了超热分子束照射,其中包含原子氧和分子氧,以研究它们的抗AO性能,并进行了分子束 - 表面散射研究,以表征原始表面和AO暴露表面上的气体 - 表面散射动力学,从而为阻力预测提供依据。AlOₓ ALD涂覆薄膜的AO侵蚀产率基本为零。基于观察到的散射动力学对代表性卫星结构的阻力模拟表明,在卫星外部表面使用AlOₓ ALD涂覆的POSS - 聚酰亚胺有潜力将阻力降低至预测的漫反射散射表面阻力的一半以下。因此,这些光滑且抗AO的聚合物薄膜在VLEO的极端氧化和高阻力环境中显示出应用前景。