Lemmon M T, Lorenz R D, Rabinovitch J, Newman C E, Williams N R, Sullivan R, Golombek M P, Bell J F, Maki J N, Vicente-Retortillo A
Space Science Institute Boulder CO USA.
Applied Physics Laboratory Laurel MD USA.
J Geophys Res Planets. 2022 Dec;127(12):e2022JE007605. doi: 10.1029/2022JE007605. Epub 2022 Dec 20.
Martian atmospheric dust is a major driver of weather, with feedback between atmospheric dust distribution, circulation changes from radiative heating and cooling driven by this dust, and winds that mobilize surface dust and distribute it in the atmosphere. Wind-driven mobilization of surface dust is a poorly understood process due to significant uncertainty about minimum wind stress and whether the saltation of sand particles is required. This study utilizes video of six Ingenuity helicopter flights to measure dust lifting during helicopter ascents, traverses, and descents. Dust mobilization persisted on takeoff until the helicopter exceeded 3 m altitude, with dust advecting at 4-6 m/s. During landing, dust mobilization initiated at 2.3-3.6 m altitude. Extensive dust mobilization occurred during traverses at 5.1-5.7 m altitude. Dust mobilization threshold friction velocity of rotor-induced winds during landing is modeled at 0.4-0.6 m/s (factor of two uncertainty in this estimate), with higher winds required when the helicopter was over undisturbed terrain. Modeling dust mobilization from >5 m cruising altitude indicates mobilization by 0.3 m/s winds, suggesting nonsaltation mechanisms such as mobilization and destruction of dust aggregates. No dependence on background winds was seen for the initiation of dust lifting but one case of takeoff in 7 m/s winds created a track of darkened terrain downwind of the helicopter, which may have been a saltation cluster. When the helicopter was cruising at 5-6 m altitude, recirculation was seen in the dust clouds.
火星大气尘埃是天气变化的主要驱动因素,大气尘埃分布、由这种尘埃驱动的辐射加热和冷却导致的环流变化以及将地表尘埃扬起并散布在大气中的风之间存在反馈作用。由于最小风应力以及沙粒跳跃是否必要存在重大不确定性,风力驱动的地表尘埃扬起过程尚不清楚。本研究利用“机智号”直升机六次飞行的视频来测量直升机上升、穿越和下降过程中的尘埃扬起情况。起飞时尘埃扬起持续到直升机超过3米高度,尘埃以4 - 6米/秒的速度平流。着陆时,尘埃扬起在2.3 - 3.6米高度开始。在5.1 - 5.7米高度的穿越过程中发生了广泛的尘埃扬起。着陆时旋翼诱导风的尘埃扬起阈值摩擦速度建模为0.4 - 0.6米/秒(该估计存在两倍的不确定性),当直升机在未受干扰的地形上空时需要更高的风速。对超过5米巡航高度的尘埃扬起进行建模表明,0.3米/秒的风就能扬起尘埃,这表明存在非跳跃机制,如尘埃聚集体的扬起和破坏。尘埃扬起的开始未发现依赖背景风,但有一次在7米/秒风速下起飞的情况,直升机顺风方向出现了一条变黑的地形轨迹,这可能是一个跳跃簇。当直升机在5 - 6米高度巡航时,在尘埃云中观察到了再循环现象。