Q³Sat: quantum communications uplink to a 3U CubeSat: feasibility and design (Conference Presentation)

S. P. Neumann, S. Joshi, Matthias Fink, T. Scheidl, R. Blach, C. Scharlemann, Sameh Abouagaga, Daanish Bambery, E. Kerstel, M. Barthélémy, R. Ursin
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Abstract

In the absence of technically mature quantum repeaters, losses in optical fibers limit the distance for ground-bound quantum key distribution. One way to overcome these losses is via optical links to satellites, which has been demonstrated in course of the Chinese-Austrian QUESS mission. Though its findings were impressive, such a large-scale project requires massive financial and time resources. We propose a 32x10x10cm³ nanosatellite orders of magnitude cheaper which is able to perform quantum key distribution (QKD) in a trusted-node scenario, using only commercially available components. We have performed a detailed analysis of such a CubeSat mission (“Q³Sat”), finding that cost and complexity can be reduced by sending the photons from ground to satellite, i.e. using an uplink. Calculations have been done for a prepare-and-send protocol (BB84 with decoy pulses) and for a protocol exploiting quantum entanglement (E91), both using polarization as information carrier. We specified the minimum requirements for the sender stations for these two different protocols. Possible orbits have been assessed, regarding both height and ellipticity to maximize link time and minimize losses. Using long-term weather data, we developed a beam model taking into account absorption, turbulence-induced beam divergence and pointing stability of sender and receiver telescope. Using light pollution measurements from space and their spectra, we arrive at maximum expectable noise count rates. We also specify the requirements for clock stability, classical communication speed and computing requirements. Incorporating all these parameters into our model, we arrive at a link budget which we can use to calculate the expected quantum secure key rates. We have also created a preliminary design of such a 3U CubeSat including a detailed size, weight and power budget and a CAD to account for the assembly of the components. Deploying a 10 cm long mirror telescope covering the small surface of the satellite leaves enough space for a polarization analysis module and housekeeping, communication and computing electronics. Polarization analysis can be done via a polarizing beam splitter and single-photon detectors with a cross section small enough to rule out radiation damage. Pointing stability and detumbling is crucial especially for such a small satellite and can be achieved via spinning wheels, achieving a precision in the tilt and yaw axis of 40 mrad. For one such CubeSat, we estimate the quantum secure key to be acquired between two ground stations during one year to be about 13 Mbit when deploying a decoy protocol. A Bell test between ground and satellite would also be feasible. The uplink design allows to keep the more sensitive, computation-intensive and expensive devices on ground. The experiment proposed by us therefore poses a comparably low-threshold quantum space mission. For a two-year lifetime of the satellite, the price per kilobit would amount to about 20 Euro. In large constellations, Q³Sats could be used to establish a global quantum network, which would further lower the cost. Summarizing, our detailed design and feasibility study can be readily used as a template for global-scale quantum communication.
Q³Sat: 3U立方体卫星的量子通信上行链路:可行性与设计(会议报告)
在没有技术成熟的量子中继器的情况下,光纤的损耗限制了地面量子密钥分发的距离。克服这些损失的一种方法是通过与卫星的光学连接,这已经在中国-奥地利QUESS任务过程中得到了证明。尽管研究结果令人印象深刻,但如此大规模的项目需要大量的资金和时间资源。我们提出了一种价格便宜的32x10x10cm³纳米卫星,它能够在可信节点场景中执行量子密钥分发(QKD),仅使用市售组件。我们对这样的CubeSat任务(“Q³Sat”)进行了详细的分析,发现可以通过将光子从地面发送到卫星(即使用上行链路)来降低成本和复杂性。已经对准备-发送协议(带有诱饵脉冲的BB84)和利用量子纠缠的协议(E91)进行了计算,两者都使用极化作为信息载体。我们为这两种不同的协议指定了发送站的最低要求。根据高度和椭圆度对可能的轨道进行了评估,以最大限度地延长连接时间并减少损失。利用长期气象数据,建立了考虑吸收、湍流引起的光束发散和收发望远镜指向稳定性的光束模型。利用来自太空的光污染测量及其光谱,我们得到了最大的预期噪声计数率。我们还详细说明了时钟稳定性、经典通信速度和计算要求。将所有这些参数纳入我们的模型,我们得到一个链路预算,我们可以用它来计算预期的量子安全密钥速率。我们还创建了这样一个3U立方体卫星的初步设计,包括详细的尺寸,重量和功率预算以及用于组件组装的CAD。在卫星的小表面上部署一个10厘米长的镜面望远镜,留出足够的空间用于偏振分析模块和管家、通信和计算电子设备。偏振分析可以通过偏振分束器和单光子探测器进行,其横截面足够小,可以排除辐射损伤。指向稳定性和下降是至关重要的,特别是对于这样一个小卫星,可以通过旋转轮来实现,在倾斜和偏航轴上实现40英里/小时的精度。对于一颗这样的立方体卫星,我们估计在部署诱饵协议时,两个地面站在一年内获得的量子安全密钥约为13 Mbit。在地面和卫星之间进行贝尔测试也是可行的。上行链路设计允许将更敏感、计算密集型和昂贵的设备留在地面上。因此,我们提出的实验提出了一个相对低门槛的量子空间任务。卫星的寿命为两年,每千比特的价格约为20欧元。在大型星座中,Q³Sats可用于建立全球量子网络,这将进一步降低成本。总之,我们的详细设计和可行性研究可以很容易地作为全球尺度量子通信的模板。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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