基于跨尺度力平衡与万物统一场频公式的大气层内火箭高效推进方案

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Authors: ZhenFeng BIAN
Cited by: 0

Abstract

中文摘要 针对传统火箭大气层内推进“喷流-空气动量传递效率低、能量损耗大”的核心痛点,提出一种基于等离子体“动态刚性借力墙”的高效推进方案。该方案以跨尺度力平衡模型(短程排斥-中程吸引)为刚性控制逻辑,以卞氏万物统一场频公式为量化工具,通过定向激光电离周边介质并结合磁场约束,在火箭喷口后方动态生成高密度等离子体墙,将喷流动量传递效率从传统的15%提升至95%以上。以200吨级火箭“地球表面→近地轨道(0-200km)”运输为场景,推导得到三段式适配参数:场频3×10¹³~6×10¹³Hz、等离子体粒子间距2.01×10⁻⁷~2.05μm、脉冲式平均能量消耗1.0×10⁶~1.3×10⁶W,最终实现推力增益≈6.1倍、燃料节能77%的性能提升。方案核心逻辑、场景应用与落地路径均属首创,所有参数可直接对接我国现有激光、超导、航天集成工程能力,相关表述贴合工程技术语境,为大气层内高效航天运输提供“理论可依、参数可算、设备可选、步骤可行”的全新技术路径。 Abstract To address the core pain points of traditional rocket propulsion in the atmosphere—low momentum transfer efficiency between jet and air, and high energy loss—an efficient propulsion scheme based on a plasma "dynamic rigid force-aided wall" is proposed. Taking the cross-scale force balance model (short-range repulsion and medium-range attraction) as the rigid control logic and Bian's universal field frequency formula as the quantitative tool, the scheme dynamically generates a high-density plasma wall behind the rocket nozzle through directional laser ionization of surrounding media combined with magnetic field confinement, increasing the jet momentum transfer efficiency from the traditional 15% to over 95%. Taking the transportation of a 200-ton-class rocket from the Earth's surface to low Earth orbit (0-200km) as the scenario, three-stage adaptive parameters are derived: field frequency 3×10¹³~6×10¹³Hz, plasma particle spacing 2.01×10⁻⁷~2.05μm, and pulsed average energy consumption 1.0×10⁶~1.3×10⁶W. Finally, a thrust gain of ≈6.1 times and a fuel saving of 77% are achieved. The core logic, scenario application, and implementation path of the scheme are original. All parameters can be directly connected to China's existing laser, superconducting, and aerospace integration engineering capabilities, and the relevant expressions are consistent with the engineering and technical context. This provides a new technical path for efficient atmospheric space transportation that is "theoretically reliable, parameter-calculable, equipment-selectable, and step-feasible."

Fields of Study & Subjects

Plasma and Flow Control in Aerodynamics Spacecraft Dynamics and Control Space Satellite Systems and Control

Publication details

Journal / source
Zenodo (CERN European Organization for Nuclear Research)
Publication date
3 January 2026
Language
ZH
Document type
Preprint