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UPDATE ON RISK REDUCTION ACTIVITIES FOR A LIQUID ADVANCED BOOSTER FOR NASA'S SPACE LAUNCH SYSTEM

机译:用于NASA空间发射系统的液体先进助推器的风险降低活动

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The stated goals of NASA's Research Announcement for the Space Launch System (SLS) Advanced Booster Engineering Demonstration and/or Risk Reduction (ABEDRR) are to reduce risks leading to an affordable Advanced Booster that meets the evolved capabilities of SLS and enable competition by mitigating targeted Advanced Booster risks to enhance SLS affordability. Dynetics, Inc. and Aerojet Rocketdyne (AR) formed a team to offer a wide-ranging set of risk reduction activities and full-scale, system-level demonstrations that support NASA's ABEDRR goals. During the ABEDRR effort, the Dynetics Team has modified flight-proven Apollo-Saturn F-l engine components and subsystems to improve affordability and reliability (e.g., reduce parts counts, touch labor, or use lower cost manufacturing processes and materials). The team has built hardware to validate production costs and completed tests to demonstrate it can meet performance requirements. State-of-the-art manufacturing and processing techniques have been applied to the heritage F-l, resulting in a low recurring cost engine while retaining the benefits of Apollo-era experience. NASA test facilities have been used to perform low-cost risk-reduction engine testing. In early 2014, NASA and the Dynetics Team agreed to move additional large liquid oxygen/kerosene engine work under Dynetics' ABEDRR contract. Also led by AR, the objectives of this work are to demonstrate combustion stability and measure performance of a 500,000 lbf class Oxidizer-Rich Staged Combustion (ORSC) cycle main injector. A trade study was completed to investigate the feasibility, cost effectiveness, an'd technical maturity of a domestically-produced engine that could potentially both replace the RD-180 on Atlas V and satisfy NASA SLS payload-to-orbit requirements via an advanced booster application. Engine physical dimensions and performance parameters resulting from this study provide the system level requirements for the ORSC risk reduction test article.
机译:NASA的空间发射系统(SLS)高级增压工程示范和/或风险减少(ABEDRR)的指定目标是降低导致一个经济实惠的高级助推器的风险,以满足SLS的进化能力,并通过减轻目标实现竞争提高SLS负担能力的先进助推器风险。 Dynics,Inc。和Aerojet Rocketdyne(AR)组建了一个团队,提供了一个广泛的风险减少活动和全面的系统级演示,支持NASA的ABEDRR目标。在Abedrr努力期间,Dynetics团队已经修改了飞行验证的Apollo-Saturn F-L发动机组件和子系统,以提高可用性和可靠性(例如,减少零件计数,触摸劳动或使用较低的成本制造工艺和材料)。该团队已建立硬件以验证生产成本并完成测试以证明它可以满足性能要求。最先进的制造和加工技术已应用于遗产F-L,导致低重复的成本发动机,同时保留了Apollo-ERA经验的好处。美国宇航局试验设施已被用于执行低成本的风险减少发动机测试。 2014年初,美国宇航局和Dynetics团队同意在Dometics的Abedrr合同下移动额外的大型液体氧/煤油引擎工作。这项工作的目标也是由AR领导,展示燃烧稳定性和测量性能的500,000 LBF型氧化剂的分阶段燃烧(ORSC)循环主喷射器。完成了贸易研究以调查可行性,成本效益,国产发动机的技术成熟度,这些发动机可能会替换ATLAS V上的RD-180,并通过先进的助推器满足NASA SLS有效载荷对轨道要求应用。该研究产生的发动机物理尺寸和性能参数为orsc风险降低测试制品提供了系统级要求。

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