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The Bridge to Space: Elevator Sizing Performance Analysis

机译:通往太空的桥梁:电梯选型和性能分析

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The Bridge to Space (BTS), an advanced system concept designed to significantly reduce payload-to-space delivery costs, consists of two major elements as seen in Figure 1: a long Space Elevator cable structure and an aircraft-like Sub-Orbital launch vehicle (SOLV). Preliminary estimates indicate the BTS can meet a launch cost target of $100/lb for 3rd generation launch systems. Previous papers have described the operational concept for launching payloads with the Bridge to Space (Marshall & Mottinger, 2000). These operations include payload transfer from the SOLV to the Space Elevator's Earth Transfer Station (ETS), payload translation along the elevator with a moving carriage platform and processing/transfer/release of the payload at the elevator's Apex Station (AS) as required, or payload release at the uppermost point of the elevator, the Space Transfer Station (STS). This paper will focus on sizing and performance modeling of the Space Elevator segment of the overall Bridge to Space. An elevator model has been developed to accept varying input parameters to determine outputs such as elevator mass and length, and altitude change/reboost requirements during payload transfer operations. Some of the key input variables include payload mass, ETS altitude and handoff velocity with the SOLV, and cable stress/density ratio. Sensitivity analyses have been performed with the model to determine the optimum altitude, velocity and size of the elevator for a given payload mass. Preliminary results of these sensitivity analyses are presented. The paper also includes a discussion of alternate concepts for the Space Elevator that could improve performance (i.e., minimize reboost fuel usage), based upon results of the model described above. Specifically, techniques to reduce the aerodynamic drag of the elevator's lower end and reduction of the overall elevator length and mass are discussed. The paper concludes with a summary of key results and lists technology development areas that would improve elevator performance.
机译:太空桥(BTS)是一种旨在显着降低有效载荷到太空的交付成本的先进系统概念,如图2所示,它由两个主要元素组成:较长的太空电梯电缆结构和类似飞机的亚轨道发射车辆(SOLV)。初步估算表明,BTS可以满足第三代发射系统100美元/磅的发射成本目标。先前的论文描述了使用太空桥发射有效载荷的操作概念(Marshall&Mottinger,2000)。这些操作包括将有效载荷从SOLV传输到太空电梯的地球传输站(ETS),使用移动的运输平台沿着电梯进行有效载荷转换以及根据需要在电梯的Apex站(AS)处理/传输/释放有效载荷,或者电梯最高处的空间转移站(STS)释放有效载荷。本文将重点讨论整个太空桥梁的空间电梯部分的尺寸和性能建模。已经开发出一种电梯模型,可以接受变化的输入参数来确定输出,例如电梯的质量和长度,以及有效载荷传输操作期间的海拔变化/重新增压要求。一些关键的输入变量包括有效载荷质量,ETS高度和带有SOLV的越区切换速度,以及电缆应力/密度比。该模型已进行了灵敏度分析,以确定给定有效负载质量的最佳电梯高度,速度和尺寸。给出了这些敏感性分析的初步结果。本文还基于上述模型的结果,对空间电梯的替代概念进行了讨论,这些概念可以提高性能(即,最小化再增压燃料的使用)。具体而言,讨论了减少电梯下端的空气阻力以及减少电梯的整体长度和质量的技术。本文最后总结了关键结果,并列出了可改善电梯性能的技术开发领域。

著录项

  • 来源
    《》|2002年|p.286-290|共5页
  • 会议地点 Albuquerque NM(IS);Albuquerque NM(IS);Albuquerque NM(IS);Albuquerque NM(IS);Albuquerque NM(IS);Albuquerque NM(IS)
  • 作者单位

    Lockheed Martin Space Systems ― Astronautics Operations PO Box 179 Denver, CO 80201;

  • 会议组织
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 V5;
  • 关键词

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