IEEE International Conference on Space Optical Systems and Applications (ICSOS)
Integration of a Polarization based QKD Receiver Module to an Optical Ground Station
R. Singh, Thomas Roger, Chithrabhanu Perumangatt, Robert I. Woodward, O. Crampton, C. Simmons, A. Green, Ross J. Donaldson, R. S. Tessinari, R. M. Stevenson, A. J. Shields
Satellite-to-ground quantum key distribution (QKD) has the potential to extend the reach of quantum secured communication to global scale. Taking the first step towards QKD using the UK quantum communication hub’s optical ground station (HOGS), this work presents results from a free-space QKD experiment conducted using the HOGS facility. A compact receiver module was integrated to HOGS and polarization encoded quantum bits, sent from a 2U QKD source, were detected, generating secret keys with total loss of up to 38 dB.
Satellite-to-ground quantum key distribution (QKD) has the potential to extend the reach of quantum secured communication to global scale. Taking the first step towards QKD using the UK quantum communication hub’s optical ground station (HOGS), this work presents results from a free-space QKD experiment conducted using the HOGS facility. A compact receiver module was integrated to HOGS and polarization encoded quantum bits, sent from a 2U QKD source, were detected, generating secret keys with total loss of up to 38 dB.
Quantum key distribution (QKD) is a provably secure key growth protocol which is resistant to powerful decryption, including increasingly powerful quantum computers, by providing a mechanism to detect eavesdropping. Satellite quantum key distribution (SatQKD) has been demonstrated for providing long-distance and mobile QKD links, but so far has required large satellites. However, we anticipate that the Hub Optical Ground Station (HOGS) is capable of demonstrating SatQKD from its partner 12U CubeSat (SPOQC, the space platform for optical quantum communications), and have developed a simulator to test the effects of link geometry and environment. This accounts for the high link loss (up to 50dB) and limited key rates (~100bits/s). To do so, HOGS must provide several support systems to maintain the satellite quantum link. By virtue of its large satellite-tracking telescope and support systems, HOGS can be an asset to a wide range of fields. The tools available for precise timing, fibre networking and satellite tracking lend themselves to research in optical communications, space engineering and quantum networking.
Quantum key distribution (QKD), the technology to generate distant secure keys for later usage in secure communication, has become a mature topic since the 1980s. While terrestrial QKD over fiber networks is suitable for short-distance urban networks, QKD via satellites promises to gap the distance requirement on a global scale that limits terrestrial QKD. Satellite QKD requires the exchange of quantum states between a satellite and multiple ground stations. The goal is then to facilitate shared secret keys between the ground stations, which can then be relayed to users near the ground stations. The satellite usually carries the quantum sources as its payload and sends them to the ground station via a downlink. The QKD protocol is heavily influenced by the choice of the quantum source, with typically one of two types: approximate single photon source (such as a weak laser) or an entangled source. Similarly, the ground station must be equipped to receive, measure and process the quantum signals sent by the satellite. Although there are also reverse schemes, where the satellite acts as the receiver and the ground station as the sender, these schemes are less explored due to higher noise in the uplink and less engineering experience. As with any system containing a high heterogeneity, many different implementation schemes lead to a variety of optimized use cases based on different criteria. Satellite QKD carries the further complication that it must be adapted to international standards. In this paper we present different satellite and ground station architectures that lean on the developments in the projects EAGLE-1, QUBE, QuNET, RoGloQuaN, addressing different protocols, sources, satellite sizes and telescope sizes. We also discuss the need for agility and configuration of components in a heterogeneous environment.
Quantum Key Distribution (QKD) is a promising method to guarantee future-proof, information theoretic security. Since optical fibers have an exponential loss with distance, satellite-based QKD solutions are being developed in order to realize long-distance links. Therefore, Optical Ground Stations for QKD (QKD-OGS) need to be designed to enable quantum communication with satellites. Different link configurations will result in different integration options of the QKD-OGS in the terrestrial fiber network and therefore impact its performance. Applicable integration options must be identified and trade-off analysis conducted at the architecture, system and sub-system level. The reference scenario is a Low Earth Orbit (LEO) downlink configuration employing a decoy-state BB84 protocol with polarization encoded qubits at 1550 nm wavelength. The satellite acts as trusted node for implementation of the key distribution between two parties on ground. Furthermore, only direct connections from the satellite to the end-users are considered, i.e. the QKD-OGS does not serve as a trusted-node relay. This results in the selection of three main integration concepts: first, a free-space, end-user QKD-OGS which is located directly at the end-user where the quantum signal is measured directly behind the receiver telescope in free-space; second, a fiber-coupled, end-user QKD-OGS where the quantum signal is coupled into a single-mode fiber and guided to a co-located server room hosting the QKD Receiver system; third, a fiber-coupled, provider QKD-OGS, which reaches several end-users by using a local fiber network. In order to evaluate these three concepts, the comparison parameter is defined to be an estimated factor of suppliable end-users. The estimated comparison factor shows that the fiber-coupled, enduser QKD-OGS can supply 6.7 times more end users than the free-space, end-user QKD-OGS. The fiber-coupled, end-user QKD-OGS can supply 129.7 times more end-users than the free-space, end-user QKD-OGS.
Satellite-based quantum key distribution (QKD) holds the potential to establish global quantum communication networks. While satellite QKD has been demonstrated using polarization encoding, time-bin encoding offers distinct advantages, such as simplifying polarization-maintaining telescope designs and being insensitive to satellite-ground relative motion. In this work, we developed a 625-MHz QKD light source using a robust Sagnac-interferometer-based modulation scheme and subsequently demonstrated time-bin QKD over a 7 km urban terrestrial free-space channel. This experiment successfully operated over a channel traversing an equivalent atmospheric thickness and loss exceeding that of typical satellite-to-ground links, achieving a low quantum bit error rate of 0.87% and a secure key rate of 134 bps@51.4 dB. Furthermore, by using a half-wave plate to simulate the polarization-basis-rotation inherent in such links, we verified the robustness of time-bin encoding for satellite scenarios. The results validate time-bin encoding as a compelling alternative and lay the technical foundation for future satellite QKD applications.
Abstract Satellite-based quantum terminals are a feasible way to extend the reach of quantum communication protocols such as quantum key distribution (QKD) to the global scale. To that end, prior demonstrations have shown QKD transmissions from airborne platforms to receivers on ground, but none have shown QKD transmissions from ground to a moving aircraft, the latter scenario having simplicity and flexibility advantages for a hypothetical satellite. Here, we demonstrate QKD from a ground transmitter to a receiver prototype mounted on an airplane in flight. We have specifically designed our receiver prototype to consist of many components that are compatible with the environment and resource constraints of a satellite. Coupled with our relocatable ground station system, optical links with distances of 3–10 km were maintained and quantum signals transmitted while traversing angular rates similar to those observed of low-Earth-orbit satellites. For some passes of the aircraft over the ground station, links were established within 10 s of position data transmission, and with link times of a few minutes and received quantum bit error rates typically ≈3%–5% , we generated secure keys up to 868 kb in length. By successfully generating secure keys over several different pass configurations, we demonstrate the viability of technology that constitutes a quantum receiver satellite payload and provide a blueprint for future satellite missions to build upon.
The low-cost small aperture commercial optical ground stations (OGSs) will play an important role in the realization of a global scale satellite-to-ground quantum key distribution (QKD) networks. OGSs with < 60 cm diameter telescope and a small mount, can have stringent size and weight limits on the payload that can be accommodated. In order to ensure easy integration with an OGS, we have designed and produced a 40×30×10 cm receiver module which comprises polarization detection optics, fine point and track (PAT) subsystem and coarse wavelength division multiplexing optics for receiving optical signals over the visible, near-infrared and infrared spectrum. The tracking capability of the module to track multiple beams of different wavelength is evaluated in an emulated beam-wander induced free-space link. The receiver module is characterized for transmission loss and polarization extinction ratio (PER) by sending an 844 nm collimated beam to the module in a 3 m free-space link and measuring the power coupled into the four single mode fibers (SMF) for H, V, D and A polarized components. Furthermore, we have used the receiver module in our satellite-to-ground QKD emulator and have measured the secure key that can be generated within different maximum elevation satellite overpasses when the quantum signal is coupled into AR-coated SMF. Such modules can be incorporated into optical ground stations (OGS) to mitigate atmospheric beam-wandering and coarse misalignment while allowing wavelength division multiplexing of multiple visible, near-infrared and infrared beams to enable co-propagation of classical and quantum communication beams for real-time QKD.