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校核推进一级假设（SFC/TSFC/η）是否可用于航程与重量闭合。当总体闭环需要推进输入或航程/燃油异常时调用。
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Based on SOC occupation classification
执行包含高级分析与机身几何的固定翼总体设计流程。初步分析收敛后调用，含高级分析、几何约束与机身外形。
固定翼总体设计唯一入口：执行 Class I 闭环并在收敛后进入阶段 2–7 扩展分析，落盘输出报告/数据/外形资产，并可选 PySide6 实时可视化。
生成固定翼总体设计方案（需求→约束→设计点→初步尺寸→重量/性能闭合）。当需要给出固定翼总体方案、关键参数范围与决策依据时调用。
| name | fixed_wing_propulsion_runbook |
| description | 校核推进一级假设（SFC/TSFC/η）是否可用于航程与重量闭合。当总体闭环需要推进输入或航程/燃油异常时调用。 |
| stage | class2_preliminary |
| code_module | aircraft_design/class2_preliminary/propulsion.py |
| dependencies | ["fixed_wing_propulsion_spec"] |
fixed_wing_overall_sizing_runbook 闭环驱动，不建议作为独立入口。sfc_1_s、prop_efficiencytsfc_1_ssfc/tsfc 单位不一致：本仓库倾向使用 1/s（例如 0.8/3600 ≈ 2.22e-4 1/s）kg/(N·h) 或 lb/(lbf·h) 直接当 1/s 用，导致航程/燃油严重异常fixed_wing_overall_sizing_runbook