针对我国新一代运载火箭“运载效率偏低、发射成本高、垂直回收姿控难”的核心瓶颈,依托“宇宙能量场震动频率统一理论(V2.0)”“粒子确定态”理论与“跨尺度力统一模型”新物理体系,提出“飞秒激光增强型环形等离子体动态墙+余热闭环供能+推力舵式姿控+多星球场景适配”的创新推进方案。方案深度整合国内成熟航天技术,通过飞秒激光参数优化、微结构靶材耦合、多场景参数拓展,在V2.0基础上实现电离效率提升至58%-60%、推力增益稳定6.5倍、能耗再降8%,同时新增月球/火星稀薄大气适配能力。核心指标均对接我国现有激光、超导、航天集成工程能力,形成“理论自洽、参数精准、设备可选、多场景适配”的完整技术体系,为200吨级运载火箭、超重型火箭(CZ-9)及多星球探测任务提供高效、低成本、可落地的推进解决方案。 English Abstract Aiming at the core bottlenecks of China's new-generation launch vehicles, such as low transportation efficiency, high launch costs, and difficulty in vertical recovery attitude control, this study proposes an innovative propulsion scheme of "femtosecond laser-enhanced annular plasma dynamic wall + waste heat closed-loop energy supply + thrust rudder-type attitude control + multi-planet scenario adaptation" based on the new physical system including "Unified Theory of Cosmic Energy Field Vibration Frequency (V2.0)", "Particle Deterministic State" theory, and "Cross-Scale Force Unified Model". Deeply integrating mature domestic aerospace technologies, the scheme achieves an ionization efficiency of 58%-60%, a stable thrust gain of 6.5 times, and an additional 8% reduction in energy consumption compared with V2.0 through femtosecond laser parameter optimization, microstructured target coupling, and multi-scenario parameter expansion. Meanwhile, it adds the adaptation capability to the thin atmospheres of the Moon and Mars. All core indicators are aligned with China's existing laser, superconducting, and aerospace integration engineering capabilities, forming a complete technical system characterized by "theoretical self-consistency, precise parameters, optional equipment, and multi-scenario adaptation". This scheme provides an efficient, low-cost, and implementable propulsion solution for 200-ton-class launch vehicles, super-heavy rockets (CZ-9), and multi-planet exploration missions.