SBIR Phase I: Liquid Oxygen (LOX) - Methane Engine for Small Satellite Launch Vehicles

SBIR 第一阶段：液氧 (LOX) - 小型卫星运载火箭的甲烷发动机

• 批准号: 2050703
• 负责人: Maksud Ismailov
• 金额: $ 25.6万
• 依托单位: ROCKET PROPULSION SYSTEMS LLC
• 依托单位国家: 美国
• 项目类别: Standard Grant
• 财政年份: 2021
• 资助国家: 美国
• 起止时间: 2021-11-01 至 2022-10-31
• 项目状态: 已结题
• 来源: https://www.nsf.gov/awardsearch/showAward?AWD_ID=2050703&HistoricalAwards=false
• 关键词: SBIR; Phase; Liquid; Oxygen; LOX

The broader impact/commercial potential of this Small Business Innovation Research (SBIR) Phase I project is to significantly lower the capital barriers for new enterprises to participate as small satellite launchers and service providers, by offering high-performance rocket engines produced at the $100 K cost point. On the production side, this change would lead to a restructuring of space launch and satellite sector supply chains from the current high cost/low volume to a low-cost/high volume configuration as in the aircraft or automotive industries. Such a change could also provide a significant increase in high paying aerospace engineering and manufacturing jobs. On the customer end, once the small satellites reach the orbit, they could expand capabilities for military and civilian services in space, from surveillance and weather monitoring to completely new industries such as agricultural earth observation and climate change monitoring, or when combined into large constellations, provide wireless and mobile internet service globally to underserved populations. This Small Business Innovation Research (SBIR) Phase I project will boost the development of American-made, high-performance, reliable, high thrust-to-weight and low maintenance liquid rocket engines of 1.5-metric-ton thrust for small 50-180 kg satellite launch vehicles to 700 km Low Earth Orbit (LEO), using low-cost liquid oxygen (LOX) / methane (or liquified natural gas) propellants. A two-stage rocket would be propelled by a cluster of six such engines on its 1st stage, and a single vacuum-version of this engine on its upper stage. The small satellite business has been growing exponentially in the last few years, with the launch demand far outpacing supply. The annual demand/supply launch gap is expected to be in the 200-700 satellite range by 2026. The primary objectives of Phase I are to design and build the preburner and thrust chamber assembly and to design the turbopump assembly. The results from Phase I will provide data on the initial engine weight, manufacturability, production cost, and define the pace, risk posture, and resource needs for engine development.This award reflects NSF's statutory mission and has been deemed worthy of support through evaluation using the Foundation's intellectual merit and broader impacts review criteria.

该小型企业创新研究 (SBIR) 第一阶段项目的更广泛影响/商业潜力是通过提供以 10 万美元生产的高性能火箭发动机，显着降低新企业作为小型卫星发射器和服务提供商参与的资本壁垒成本点。 在生产方面，这一变化将导致航天发射和卫星行业供应链的重组，从目前的高成本/低产量配置转向飞机或汽车行业的低成本/大产量配置。 这种变化还可能导致高薪航空航天工程和制造工作岗位的大幅增加。在客户端，一旦小型卫星到达轨道，它们就可以扩展太空军事和民用服务的能力，从监视和天气监测到农业地球观测和气候变化监测等全新行业，或者组合成大型星座，为全球服务不足的人群提供无线和移动互联网服务。 该小型企业创新研究 (SBIR) 第一阶段项目将促进美国制造、高性能、可靠、高推重比和低维护的 1.5 吨推力液体火箭发动机的开发，适用于小型 50-180 英里千克卫星运载火箭飞往 700 公里低地球轨道 (LEO)，使用低成本液氧 (LOX)/甲烷（或液化天然气）推进剂。两级火箭将由第一级上的六台此类发动机驱动，而上级上则由该发动机的单个真空版本驱动。 过去几年，小型卫星业务呈指数级增长，发射需求远远超过供应。 预计到 2026 年，每年的发射需求/供应缺口将在 200-700 颗卫星范围内。第一阶段的主要目标是设计和建造预燃器和推力室组件以及设计涡轮泵组件。第一阶段的结果将提供有关初始发动机重量、可制造性、生产成本的数据，并确定发动机开发的节奏、风险状况和资源需求。该奖项反映了 NSF 的法定使命，并通过使用评估结果被认为值得支持。基金会的智力价值和更广泛的影响审查标准。