Capsulation satellite or CapSat: A low-cost, reliable, rapid-response spacecraft platform

J. Burt, D. Steinfeld
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引用次数: 3

Abstract

The National Aeronautics and Space Administration (NASA) Goddard's Rideshare Office estimates that between 2013 and 2022, NASA launches of primary satellites will have left unused more than 20,371 kilograms of excess capacity. This equates to hundreds of millions of dollars in launch-vehicle costs going unutilized. To fill this void with a standard CubeSat or SmallSat spacecraft platform, which when required to be more reliable, still will cost in the neighborhood of $1M a kilogram, making it prohibitively expensive. A newly proposed solution, which NASA is pursuing, is called the Capsulation Satellite or CapSat. CapSat is a modularized, pressurized, thermally controlled spacecraft designed to host ruggedized commercially available instrumentation in a terrestriallike environment on orbit. Using a technique that is under review for a patent, CapSat actively manages internal air temperatures in a manner similar to a household thermostat. This gives CapSat high-thermal stability, which, in turn, provides component longevity. CapSat was specifically designed to take advantage of the United States Air Force (USAF) Rideshare Program and the Evolved Expendable Launch Vehicle Secondary Payload Adaptor, or ESPA ring. The ESPA ring comes in two sizes: standard and Grande. CapSat primarily will take advantage of the ESPA Grande to provide a 300-kilogram payload capability per attachment point, with up to four attachment points per ring. This approach combines a high-mass capability with a proven Rideshare mechanical interface and secondary payload management infrastructure. Opportunities for ESPA-based co-manifests are continuing to expand. The CapSat program is currently funded to design and build a limited prototype and perform thermal-vacuum testing. CapSat is currently in the concept/study phase for both single missions and constellation of earth- and space-observing missions. One of these studies includes land imaging using state-of-the-art advanced infrared detector technology. This paper will report on the current status of the CapSat hardware design, testing, and results as well as any openly available advanced concept study results. The CapSat solution is intended to be a game-changing paradigm shift. CapSat will repurpose currently available, already-proven technology to reduce spaceflight hardware costs to less than $50,000 per kilogram.
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胶囊卫星(CapSat):一种低成本、可靠、快速响应的航天器平台
美国国家航空航天局(NASA)戈达德拼车办公室估计,在2013年至2022年期间,NASA发射的主要卫星将留下超过20,371公斤的剩余容量。这相当于数亿美元的运载火箭费用没有得到利用。用标准的立方体卫星或小型卫星航天器平台来填补这一空白,当需要更可靠时,每公斤的成本仍将在100万美元左右,这使得它的成本高得令人望而却步。美国国家航空航天局(NASA)正在寻求一种新提出的解决方案,称为“太空舱卫星”(CapSat)。CapSat是一种模块化的、加压的、热控制的航天器,设计用于在轨道上的类地环境中承载加固的商用仪器。CapSat采用一项正在申请专利的技术,以类似于家用恒温器的方式主动管理内部空气温度。这为CapSat提供了高热稳定性,从而延长了组件的使用寿命。CapSat是专门为利用美国空军(USAF)拼车计划和演变的一次性运载火箭二次有效载荷适配器(ESPA环)而设计的。ESPA戒指有两种尺寸:标准和大尺寸。CapSat将主要利用ESPA Grande为每个附着点提供300公斤的有效载荷能力,每个环最多有四个附着点。这种方法将高质量性能与成熟的Rideshare机械接口和辅助有效载荷管理基础设施相结合。基于espa的共同舱单的机会正在继续扩大。CapSat项目目前的资金用于设计和建造一个有限的原型,并进行热真空测试。CapSat目前正处于单一任务和地球和空间观测任务星座的概念/研究阶段。其中一项研究包括使用最先进的红外探测器技术进行陆地成像。本文将报告CapSat硬件设计、测试和结果的现状,以及任何公开可用的先进概念研究结果。CapSat的解决方案旨在改变游戏规则。CapSat将重新利用目前可用的、已经得到验证的技术,将航天硬件成本降低到每公斤5万美元以下。
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