火星大本营:2028年将人类送上火星的建筑

T. Cichan, S. Bailey, S. Norris, R. Chambers, S. Jolly, J. Ehrlich
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引用次数: 12

摘要

“猎户座”多用途载人飞船是美国国家航空航天局(NASA)地球外轨道(BEO)人类探索架构的关键部分。洛克希德·马丁公司被授予猎户座的设计、开发、测试和生产合同,一直到探索任务2 (EM-2)。洛克希德·马丁公司也在与美国国家航空航天局合作,致力于确定顺月试验场任务架构。此外,洛克希德·马丁公司正在探索将火星任务定义为地平线目标,为人类探索太阳系的计划提供输入。本文描述了一种体系结构,以确定在大约十年内建立火星大本营体系结构的可行性。这一架构将涉及人类对火星两个卫星的探索,并为宇航员提供一个与火星上的预阶段机器人资产互动的机会。这项研究是一个高层次的评估,以确定架构驱动因素和科学机会。这个体系结构有几个关键原则。对于这第一次人类星际任务,系统冗余和自救能力是必需的。系统开发的数量被最小化,已经开发的系统如太空发射系统和猎户座的使用被最大化。为了最大限度地减少可能导致全体机组人员损失的事件的数量,该结构不需要在任务期间对机组人员生存所必需的预阶段元素进行交会和对接。本文将描述所需的不同启用技术。将描述轨道假设,包括为穿越火星和返回地球而进行的研究结果,以及探索火星系统的任务设计交易。将详细介绍转运车模块的设计概念。可能的科学活动将被描述。还将讨论推进技术、装配方法和任务活动的研究结果,以及对计划开展的工作的讨论。这项架构研究的结果将表明,近期的火星任务是令人信服和可行的,并将突出所需的关键系统。
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Mars Base Camp: An architecture for sending humans to Mars by 2028
Orion, the Multi-Purpose Crew Vehicle, is a key piece of the NASA human exploration architecture for beyond earth orbit (BEO). Lockheed Martin was awarded the contracts for the design, development, test, and production for Orion up through the Exploration Mission 2 (EM-2). Lockheed Martin is also working on defining the cis-lunar Proving Ground mission architecture, in partnership with NASA. In addition, Lockheed Martin is exploring the definition of Mars missions as the horizon goal to provide input to the plans for human exploration of the solar system. This paper describes an architecture to determine the feasibility of a Mars Base Camp architecture within about a decade. This architecture would involve human exploration of both Martian moons, and provide an opportunity for the crew to interact with pre-staged robotic assets on Mars. This study is a high-level assessment to identify architecture drivers and science opportunities. There are several key tenets for this architecture. For this first human interplanetary mission, system redundancy and a self-rescue capability is required. The number of system developments is minimized, and the use of the already developed systems like the Space Launch System and Orion is maximized. To minimize the number of events that could lead to the loss of the whole crew, the architecture does not require rendezvous and docking of pre-staged elements necessary for crew survival during the mission. This paper will describe the different enabling technologies required. The trajectory assumptions will be described, including the results of studies performed for the transit to Mars and return to Earth, in addition to mission design trades for the exploration of the Martian system. The transfer vehicle module design concept will be detailed. Possible science activities will be described. Study results for propulsion technology, assembly methods, and the mission campaign will also be addressed, as well as a discussion of planned forward work. The results of this architecture study will show that a near term Mars mission is compelling and feasible, and will highlight the required key systems.
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