论文标题
通过空中平台来表征金星云层可居住性的任务体系结构
Mission Architecture to Characterize Habitability of Venus Cloud Layers via an Aerial Platform
论文作者
论文摘要
金星以其极端的表面温度和硫酸云而闻名。但是,金星上的云层的温度和压力条件与地球表面的温度和压力条件相似,并且被认为是微观生命形式的可能栖息地。我们提出了一个任务概念,以探索金星的云层长达30天,以评估可居住性和寻找生活迹象。基线任务针对2026年的推出机会。超压可变的浮点高度气囊循环在48至60 km之间的高度之间,即主要横穿下部,中间和一部分云层层。仪器套件是由源自先锋金星大探头压力容器的吊船设计。 Aerobot通过轨道继电器与直接到地球链接结合使用数据。将轨道捕获到6小时的逆行轨道上,其倾斜度低,大约170度。轨道和入口探针的总质量估计为640千克。与可变浮动高度版本相比,还讨论了恒定浮点高度气球的替代概念。拟议的任务将补充其他计划的任务,并有助于阐明可居住性的局限性以及未知的化学作用,或者在金星大气中生命本身的作用。
Venus is known for its extreme surface temperature and its sulfuric acid clouds. But the cloud layers on Venus have similar temperature and pressure conditions to those on the surface of Earth and are conjectured to be a possible habitat for microscopic life forms. We propose a mission concept to explore the clouds of Venus for up to 30 days to evaluate habitability and search for signs of life. The baseline mission targets a 2026 launch opportunity. A super-pressure variable float altitude balloon aerobot cycles between the altitudes of 48 and 60 km, i.e., primarily traversing the lower, middle, and part of the upper cloud layers. The instrument suite is carried by a gondola design derived from the Pioneer Venus Large Probe pressure vessel. The aerobot transmits data via an orbiter relay combined with a direct-to-Earth link. The orbiter is captured into a 6-h retrograde orbit with a low, roughly 170-degree, inclination. The total mass of the orbiter and entry probe is estimated to be 640 kg. An alternate concept for a constant float altitude balloon is also discussed as a lower complexity option compared to the variable float altitude version. The proposed mission would complement other planned missions and could help elucidate the limits of habitability and the role of unknown chemistry or possibly life itself in the Venus atmosphere.