AIAA G-140-2015提供了有关当前使用的自然陆地环境标准的指南 设计和开发穿越地球大气层（0-90千米）的航空航天飞行器 海拔高度）。本指南在一个参考文献中详细介绍了 这些自然陆地环境输入的最新技术。使用的内容基于 航空航天飞行器开发经验和陆地自然环境综合指南 大量航天器开发中使用的环境。针对以下环境现象提供了航空航天飞行器设计标准指南: 风；大气模式和热力学性质；热辐射；美国和世界表面 极端；湿度降水、雾和结冰；云现象和云覆盖模型；大气的 电大气成分；航空航天飞行器排气和有毒化学物质释放；龙卷风 飓风；地质灾害；还有海州。本AIAA指南第15节和第16节基于 参考的NASA TM包括任务分析、发射前监测、飞行评估、， 物理常数和公制/英制单位换算系数。

AIAA G-140-2015 provides guidelines regarding the current natural terrestrial environment criteria for use in the design and development of aerospace vehicles traversing the terrestrial atmosphere (0?90 km altitude). This Guide specifies and provides, in one single reference, a comprehensive description of the state of the art of these natural terrestrial environment inputs. The contents to be used are based on aerospace vehicle development experiences and consolidated guidelines for natural terrestrial environments that have been utilized in a large number of space vehicle developments.Aerospace vehicle design criteria guidelines are provided for the following environmental phenomena: winds; atmospheric models and thermodynamic properties; thermal radiation; U.S. and world surface extremes; humidity; precipitation, fog, and icing; cloud phenomena and cloud cover models; atmospheric electricity; atmospheric constituents; aerospace vehicle exhaust and toxic chemical release; tornadoes and hurricanes; geologic hazards; and sea state. Sections 15 and 16 of this AIAA Guide based on the referenced NASA TM include information on mission analysis, prelaunch monitoring, flight evaluation, physical constants, and metric/English unit conversion factors.