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HEAVY LIFT LAUNCH VEHICLE SYSTEMS ARCHITECTING

机译:重型起步车辆系统架构

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As the Space Shuttle program draws to a close, NASA faces the challenge of developing thetransportation system for future human space exploration. Given current debates on the goals ofthe space program, it is critical to ensure that comprehensive but transparent exploration ofavailable options for future launch vehicle developments is available.Evaluation of launch architectures requires the assessment of options over a range ofdimensions, which can be broadly grouped into technical performance, time to initial capability,cost, and satisfaction of stakeholders' various needs. The challenge is to fairly compare a broadrange of architectures across these dimensions, in a way that empowers high level decisionmakers.This paper describes a tradespace exploration study which provides preliminary design offamilies, by exploring hundreds of concepts using coarse system evaluation metrics. The paperinvestigates the trade-offs associated with stage propellant selection, launch vehicle configurationand other relevant design parameters. Furthermore, the study considers potential LEO-classvehicles derived from the heavy lift vehicle in order to deliver early benefit from the heavy liftvehicle and provide an ongoing affordable LEO service.Architectures are evaluated through a broad set of metrics, including engineering performance,compliance to stakeholder needs and goals, compatibility with existing ground infrastructure andoff-design performance. The technical assessment methodology is validated against existinglaunch vehicles. The paper demonstrates how a field of 192 possible launch vehicles can betransparently reduced to seven possible designs on technical considerations, almost all of whichare represented by particular viewpoints in the current debate, and how further narrowing thedesign space requires weighting competing stakeholder priorities. The preferred conceptsemerging from the study are a 2.5 stage 7/8.4m diameter all-cryogenic vehicle and a 7/8.4mdiameter 2.5 stage LOX/LH2 vehicle with solid boosters as preferred baselines for furtherconceptual study. The paper further shows how conducting this coarse tradespace explorationearly in the process can inform decision-making on the future space transportation infrastructure.The paper closes with some suggestions for future work in the area.
机译:随着航天飞机计划的结束,NASA面临着开发航天飞机的挑战。 未来人类太空探索的运输系统。针对当前的目标进行辩论 在太空计划中,确保对太空进行全面而透明的探索至关重要 提供了未来运载火箭发展的可用选项。 评估启动架构需要评估以下范围内的选项: 维度,可以大致分为技术性能,开始生产所需的时间, 成本,以及利益相关者的各种需求的满意度。挑战在于公平地比较广泛 跨这些维度的一系列体系结构,以实现高层决策的方式 制造商。 本文介绍了一个贸易空间探索研究,该研究提供了初步的设计 系列,通过使用粗略的系统评估指标探索数百个概念。论文 调查与阶段推进剂选择,运载火箭配置相关的权衡 和其他相关的设计参数。此外,研究还考虑了潜在的LEO级 重型起重车辆派生的车辆,以便尽早从重型起重车辆中受益 车辆,并提供持续的负担得起的LEO服务。 通过一系列衡量指标对体系结构进行评估,包括工程性能, 符合利益相关者的需求和目标,与现有地面基础设施的兼容性以及 超出设计的性能。技术评估方法已针对现有方法进行了验证 运载工具。本文演示了如何在192种可能的运载火箭中找到一个 出于技术考虑,将其透明地简化为七个可能的设计,几乎所有这些 在当前辩论中以特定观点来代表,以及如何进一步缩小范围 设计空间需要权衡竞争的利益相关者优先级。首选概念 研究中出现的是2.5级直径7 / 8.4m的全低温载体和7 / 8.4m 直径2.5级LOX / LH2车辆,带有固体助推器,作为进一步改进的首选基准 概念研究。本文进一步展示了如何进行这种粗略的贸易空间探索 在此过程的早期,可以为未来的太空运输基础设施提供决策依据。 本文最后提出了对该地区未来工作的一些建议。

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