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A Parametric Investigation of Satellite Servicing Requirements, Revenues, and Options in Geostationary Orbit

机译:对地静止轨道卫星服务需求,收入和选择的参数研究

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A variety of viewpoints can be heard concerning the utility of on-orbit satellite servicing, the maturity of the robotic systems being developed to address servicing opportunities, and the viability of business cases. This paper seeks to quantify the opportunities and address the myths directly. Based on that analysis, we further refine servicing models using a variety of servicing vehicle parameters to identify promising configurations and missions. We review the past opportunities for geostationary Earth orbit (GEO) on-orbit servicing interventions both for unexpected anomalies and for lifetime extension. These opportunities are characterized in a number of ways, including AV for a servicer to rendezvous with the client satellite, the corrective up-mass required to perform the servicing task, the robotic degree of difficulty of accomplishing the task, and economic measures of the value of the service. Past work by two of the authors categorized satellite failures into serviceable and non-serviceable cases, and further parameterized the serviceable cases by the complexity of servicing required. After updating this database to include recent satellite failure histories, we add new dimensions to the study by characterizing serviceable failure histories by the logistics mass required to accomplish the repair. In some cases, no significant additional mass is required, such as in the case of a spacecraft requiring deployment of a stowed boom or other structural element. In other cases, consumables replenishment may require tens or hundreds of kilograms of station-keeping propellant. In still others, major systems such as photovoltaic arrays would have to be replaced to return the satellites to functionality. To provide an input into the revenue side of a cost-benefit trade, we present a revenue model for inspection and repair services, which complements revenue assessments in the literature for different services such as refueling. The episodic nature of revenues from inspection and repair missions is treated statistically. The cost side of the trade is modeled in terms of propellant consumed by the servicer. For most of the emerging servicing concepts, the notional servicing systems have delivery masses similar to or greater than the typical communications satellite servicing client spacecraft. Since the mission costs are as large or greater than a replacement satellite would be, economic viability requires a sizeable pool of satellites ready to pay for services, and willing to wait in line for servicing mission concepts, which may require the successful servicing of a number of client satellites to break even. Based on the required logistics mass and the potential revenues, the paper then seeks to examine the practicality of servicing systems at a variety of scales in terms of the relative numbers of potential servicing clients and differences in practical servicing architectures. Given existing and future client satellites that could be returned to operation with minimal logistics mass, there is a potential business case for servicing vehicles even at the smallsat class (less than 100 kg). The paper develops strawman designs for servicing systems at several different mass points, at a variety of fractions of the mass of the average geostationary communications satellite, and for candidate launch and delivery systems to allow GEO servicing. Finally, we examine in more detail various aspects of servicing, and how they differ across the scale of servicing systems. This includes issues such as small vehicles stabilizing much larger client vehicles during servicing operations, required reach capabilities between grapple points and servicing sites, and scaling of electrical power requirements with servicer size. We also model the costs of less elegant solutions to servicer deliveries: dedicated launches in the event that secondary launch approaches prove to be infeasible or unavailable, and how the greater transportation costs would affect overall economic viability.
机译:关于在轨卫星服务的实用性,为解决服务机会而开发的机器人系统的成熟度以及商业案例的可行性,可以听到各种各样的观点。本文旨在量化机会并直接解决神话。基于该分析,我们使用各种维修车辆参数进一步完善维修模型,以识别有前途的配置和任务。我们回顾了过去发生的对地静止地球轨道(GEO)轨道维修干预措施的机会,以应对意外异常和延长使用寿命。这些机会具有多种特征,包括供服务商与客户卫星会合的AV,执行服务任务所需的校正质量,完成任务的机械手难度以及价值的经济衡量方法。服务。两位作者的过去工作将卫星故障分为可维修和不可维修的情况,并根据所需维修的复杂性进一步确定了可维修的情况。在更新此数据库以包括最近的卫星故障历史记录之后,我们通过根据完成维修所需的物流量来表征可维修的故障历史记录,从而为研究增加了新的维度。在某些情况下,不需要很大的额外质量,例如在航天器中需要展开收起的起重臂或其他结构元件的情况下。在其他情况下,消耗品补给可能需要数十或数百公斤的固定站推进剂。在其他情况下,必须更换诸如光伏阵列之类的主要系统,才能使卫星恢复正常工作。为了向成本效益贸易的收益方提供输入,我们提出了检查和维修服务的收益模型,该模型补充了文献中针对不同服务(例如加油)的收益评估。从检查和维修任务中获得的收入的情节性质在统计学上得到了处理。交易的成本方面是根据服务方消耗的推进剂来建模的。对于大多数新兴的服务概念,概念服务系统的交付质量类似于或大于典型的通信卫星服务客户航天器。由于任务成本与替换卫星的成本相同或更大,因此,经济可行性要求有大量卫星准备为服务付费,并愿意排队等待为任务概念提供服务,这可能需要为许多卫星提供成功的服务客户卫星的收支平衡。根据所需的物流量和潜在收入,本文试图根据潜在服务客户的相对数量和实际服务架构的差异,研究各种规模的服务系统的实用性。考虑到现有和未来的客户卫星可以以最小的物流量重新投入运行,即使是在小卫星级别(小于100千克),也存在维修车辆的潜在商业案例。本文针对几种不同质量点,平均地球静止通信卫星质量的几分之一的服务系统以及适用于GEO服务的候选发射和传送系统,开发了稻草人设计。最后,我们将更详细地研究维修的各个方面,以及它们在整个维修系统的规模上有何不同。这包括以下问题,例如小型车辆在维修操作期间稳定了更大的客户车辆,抓斗点与维修地点之间所需的到达能力以及随维修人员规模而定的电功率需求。我们还对服务交付的不太优雅的解决方案的成本进行建模:如果辅助发射方法被证明不可行或不可用,则进行专用发射,以及更高的运输成本将如何影响总体经济生存能力。

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