Open Access

Nanosatellite experiments to enable future space-based QKD missions

EPJ Quantum Technology20163:12

DOI: 10.1140/epjqt/s40507-016-0051-7

Received: 13 July 2016

Accepted: 5 October 2016

Published: 18 October 2016


We present a programme for establishing the space worthiness of highly-miniaturised, polarisation-entangled, photon pair sources using CubeSat nanosatellites. Once demonstrated, the photon pair sources can be deployed on more advanced satellites that are equipped with optical links to establish a global space-based quantum key distribution network. In doing so, this work will also bring experimental tests of the overlap between quantum and relativistic regimes closer to realisation.



1 Introduction

Improvements in quantum computers are increasing the threat to conventional public key encryption. This is driving the development of new “quantum-safe” encryption techniques [1]. Entanglement-based quantum key distribution (QKD) is one of the possible solutions, providing security that is traceable to fundamental correlations between photons, and reducing the number of trusted components when compared with other systems. A global, space-based network for distributing entangled photons will enable strong encryption keys to be delivered securely between any two points on Earth.

Entanglement-based QKD is a mature technology. It has been demonstrated on multiple occasions and is the most established technological application of entanglement. Its range limit however is similar to more commonplace QKD schemes (such as the prepare-send-measure approach in the original proposal by Bennett and Brassard [2]). City-sized QKD networks utilising either optical fibre or free-space optics are possible, but the losses within fibres and atmospheric turbulence near the ground restrict the practical range to about a hundred kilometres. To operate on continental and global scales, it is anticipated that future quantum networks would be similar to conventional data networks and employ both fibre-based solutions (quantum-repeater-equipped) and links with optical quantum communication satellites.

Despite much discussion and many theoretical studies, getting relevant quantum technology into space has been hampered by the cost of traditional space development. At the time of writing only one conventional-sized, QKD satellite has been launched, the Chinese QUESS (QUantum Experiments at Space Scale) mission [3]. To accelerate development we are seizing on a revolution in the space industry where the use of very small spacecraft known as nanosatellites is enabling access to space for a large number of organisations with only modest funding. Recent years have seen an explosion of interest in nanosatellites, particularly CubeSats [4], where low costs and fast development times are challenging more traditional platforms for applications.

It is our goal to develop a source of entangled photons that is sufficiently bright for space-based QKD, but with a physical and resource footprint that is compatible with CubeSats. This paper presents an overview of our work towards this goal.

2 Space-based QKD

To share quantum encryption keys between space and ground the quantum key (photon) source can be located on the ground or in space [5] (see Figure 1). We (like QUESS) have chosen to focus on having the source in space from which photons are beamed to telescopes on the ground or other spacecraft. This will allow for versatility in QKD experiments (and other experiments [6]) - for example in Figure 1, three of the four QKD configuration options require a space-based source. Beaming photons from space-to-ground also has the advantage that the optical transmission path is much less affected by atmospheric turbulence (because the atmosphere is only significantly thick near the surface of the Earth) so optical link losses are lower [7], although groups have proposed various ground-to-space missions [811].
Figure 1

Scenarios for QKD in space. Possible satellite-based QKD implementations. 1. Ground-to-space, where the photon source is on the ground and the satellite only carries detectors. 2. Space-to-ground, where the satellite carries a source and detectors. 3. A platform that can beam down to two ground stations simultaneously. 4. Inter-satellite QKD which could be the building block for a long baseline test of quantum correlations. To enable configurations 2-4 with Bell violation-type measurements, a source of entangled photons in space must be demonstrated.

If scenarios 1 or 2 are used to share keys between two ground stations then it is required that the satellites be trusted as secure key exchanging nodes. However, for scenario 3 (such as the SpaceQUEST mission concept [12]) entanglement-based QKD removes that requirement for trust since if one photon in each pair of photons is beamed to Alice (at one ground station) and the other of the pair beamed to Bob (who is at the other ground station) then only Alice and Bob will have knowledge of the polarisations and the key generated is private to them. They will be able to test this quantum exclusivity by performing a Bell violation test [13]. This does of course require ground stations that are concurrently within the field-of-view of the satellite, and since both photons in a pair are travelling along high-loss paths the probability of both photons in a pair reaching their ground stations is very small and thus key generation rates would be very slow.

For most practical purposes though, it is likely that a key exchanging node satellite could be a workable solution. Although they rely on non-quantum security assurances a space-based node is difficult to access via side-channels. For example, the reported side-channel attacks on terrestrial QKD systems [14] are difficult to implement when targeting a fast-flying node where communications can only be achieved over a solid angle of tens of pico steradians.

3 CubeSat platform

We are targeting our initial satellite technology developments for use on CubeSats. These use a standardised nanosatellite specification backed by a large and growing industry of compliant subsystems and launch services all of which greatly facilitate access to space.

The smallest typical free-flying CubeSat is a 10 cm cube and is a fully-functional nanosatellite (i.e. it contains miniaturised solar panels, batteries, onboard computer, radio transceiver as well as a miniature technical or scientific payload). The CubeSat architecture allows the basic cube design (1U) to be extended into larger sized (cuboid) spacecraft measured as multiples of U (2U, 3U, 6U etc., see Figure 2). Depending on launcher and solar panel configurations each 1U might allow for 1-3 kg of spacecraft and 1-3 Watts of power.
Figure 2

3U, 2U and 1U CubeSats. Isometric CAD drawings of 3U, 2U and 1U CubeSats respectively (based on ISIS structure and GomSpace Gom-X platform).

Since the launch costs are a fraction of the cost of those for traditional spacecraft, CubeSats have become very popular with amateur researchers, university research groups and technology companies seeking a market niche. They are now also gaining popularity with older, well-established space industry players. To keep the hardware budgets small they are typically built from commercial-off-the-shelf (COTS) components rather than expensive, scarce and outdated space-grade parts. Additionally they are often launched into orbits with an orbital life of a few years or even months (although some CubeSats, like Delfi-C3 [15], have been operational now for many years). Space worthiness of COTS components can be assessed by their use in previous CubeSat missions and by carrying out targeted testing.

CubeSats typically reach orbit by ride-sharing with larger satellite launches [16] or are carried as cargo to the International Space Station (ISS) from where they are deployed into orbit [17]. This “piggy-backing” helps make launch costs affordable to university groups. As with traditional satellites, there is a further level of savings available where each CubeSat can be used to host multiple miniature research payloads. A drawback of this approach is the low duty-cycle for experiment time as the limited power on a CubeSat results in restricted operation time for each payload. Despite the limitations, we propose that it is ultimately feasible to produce pairs of entangled photons on board a CubeSat and to use these pairs to produce a shared quantum key with a ground station or another satellite. The Canadian NanoQEY mission concept meanwhile proposes an alternative ground-to-space (scenario 1 in Figure 1) approach to performing QKD with CubeSats.

Since CubeSats can be built and launched relatively inexpensively and with rapid development cycles, we have chosen to first develop and demonstrate the photon source, before attempting to beam photons to the ground. For the initial technology demonstration missions the photon pair source and the detection apparatus (Bell State analyser) will all be located inside the satellite (Figure 3). Such missions test the ability of the source to survive the vibrations and shocks of launch and investigate how it performs and ages with the ionising radiation, vacuum and thermally demanding conditions of low Earth orbit.
Figure 3

QKD precursor missions. For our first satellite missions we aim to deploy small and rugged photon pair sources on CubeSats to verify the ruggedness of the optical design and the operation of the supporting electronics. No optical link is needed in this configuration.

4 Entangled photon sources for space

For an optimal space-based QKD source the goal is to maximise key-rate and source longevity, within practical mission constraints. This means producing large rates of high-entanglement-quality photon pairs in a compact, robust package. A large number of entangled photon sources based on various physical mechanisms have been reported in the literature, but most of them are incompatible with nanosatellites due to size, weight and power (SWAP) requirements.

Accordingly, we identified sources based on Spontaneous Parametric Downconversion (SPDC) as the most promising. In this class only geometries relying on bulk crystals satisfy all the conditions needed for brightness, quality and ruggedisation. Table 1 shows a comparison of SPDC sources discussed in published literature.
Table 1

Comparison of published results of various SPDC sources



Brightness pairs/s/mm/mW

Collection efficiency %


Kwiat et al. [18]




Kwiat et al. [19]





Fiorentino [20]




Fedrizzi et al. [21]





Trojek and Weinfurter [22]




Trojek and Weinfurter [22]





Rangarajan et al. [23]




BiBo crystal

Steinlechner et al. [24]




10 μW pump

Da Cunha Pereira et al. [25]





Dixon et al. [26]





Steinlechner et al. [27]





Steinlechner et al. [27]





Septriani et al. [28]





The collection efficiency (ratio of detected pairs to single photons) of a source is an important parameter, but one that is not always quoted in papers. Entries marked * indicate sources that produce correlated photon pairs that are not entangled in polarisation.

To fit in a CubeSat, the size requirement is critical. For a 1U CubeSat an experimental payload would typically be contained in a volume that is approximately \(10~\mbox{cm}\times 10~\mbox{cm}\times 3~\mbox{cm}\). The overall mass of such an instrument should not exceed 500 g, while the continuous (peak) power consumption should be below 2.0 W (2.5 W).

Collinear SPDC geometries are favourable because non-collinear sources require a more complex (and less robust) arrangement to achieve a compatible form factor. SPDC sources based on collinear geometries typically utilise quasi-phase-matching conditions. Quasi-phase-matching, however, often involves the use of periodically-poled crystals that require precise (within 0.1 C) temperature stabilisation. Satellites in orbit experience cyclical fluctuations of temperature as they pass in and out of the Earth’s shadow, but the use of temperature stabilisation (especially with thermo-electric coolers) is challenging on CubeSats because of power and weight restrictions.

Two collinear geometries were considered: critical phase matching with Type-I β-Barium Borate (BBO) crystals [22] and a non-critical phase matching approach using Type-II periodically poled potassium titanyl phosphate (PPKTP) crystals [27]. PPKTP sources are attractive due to the higher nonlinear coefficients, better tolerances against temperature drift and the possibility of longer crystals (with fewer compensation crystals). BBO sources however have the advantage of using much cheaper crystals, as well as the ability to manufacture crystals with large apertures, making alignment and collection of downconverted light much simpler [28]. To operate with PPKTP crystals would require beam shaping optics that could not be squeezed into the smallest of the CubeSat form-factors. After considering the advantages and disadvantages of the two designs, the BBO-based source was selected for our current devices.

5 Small photon entangling quantum system (SPEQS)

The entangled photon pair sources being produced, SPEQS (Small Photon Entangling Quantum Systems), are being developed in iterative cycles that include regular on-orbit testing in CubeSats, as outlined in Table 2. The aim is to gradually raise the technology readiness level of the photon pair sources. The initial iterations developed the miniaturised electronics and ruggedised optics. These led onto on-orbit tests of a correlated photon pair source (these photons are not entangled in polarisation but may have entanglement in other degrees of freedom, e.g. time-frequency).
Table 2

Milestones leading to on-orbit QKD demonstrations






Basic miniature SPDC source

High altitude balloon test



Correlated SPDC pair source

High altitude balloon test



Space-qualified, correlated, SPDC source survives rocket explosion

GomSpace GomX-2 CubeSat



Space-qualified, correlated, SPDC source in low earth orbit

NUS Galassia CubeSat



Demonstration of entangled photon pair source in space

CQT SpooQy-1 CubeSat



Demonstration of high-brightness entangled photon pair source in space

CQT SpooQy-2 CubeSat


These missions test the space-worthiness of the devices in-situ and do not involve beaming photons outside the spacecraft. Future missions (at the time of writing) are italicised.


To address first the challenges of miniaturisation and space-proofing SPEQS-CS, a 1U-compatible, correlated photon source (with integrated polarisation analyser), has been developed. By adopting this compact format the number of flight opportunities for testing it is maximised as it can fly as a guest payload on the CubeSats of third party organisations. Although the room for optical elements is very limited, the platform is an effective solution for proving the functionality of the control electronics, and the space worthiness of the components and the mechanical assembly techniques.

A key challenge for the detection of single photons with avalanche photodiodes (APDs) is maintaining a constant detection efficiency. This is typically achieved by cooling the detectors, e.g. by using thermo-electric coolers, however these require more power than typical CubeSats can supply. By monitoring the pulse height of detection events however, the bias voltage of the APD can be continually adjusted so that its detection efficiency can be maintained in spite of changing temperatures [35].

Another challenge associated with detection is the effect of space radiation on the APDs. Accumulated radiation damage increases the rate of dark counts (thermally generated noise). This noise can be reduced by cooling the detectors but our radiation tests indicate that we should be able to perform our proof of concept demonstrations without cooling. The liquid crystal polarisation rotator performance was found to be relatively insensitive to ionising space radiation [36]. This was also true for the rest of the COTS electronics.

A key test of a SPEQS-CS was performed on a helium balloon in Switzerland [30]. The balloon reached an altitude of 35.5 km and experienced rapid temperature swings and shock loads yet our device was shown to perform nominally throughout.

A later copy was integrated onto the GomSpace GomX-2 satellite. This CubeSat was prepared for deployment from the ISS but its journey to space was cut short when the rocket it was launched on exploded shortly after lift off. Remarkably the CubeSat was recovered intact from a nearby beach. The satellite was subsequently activated and the SPEQS instrument was found to be fully operational [31]. Another variant of a SPEQS-CS was supplied and integrated onto the NUS Galassia CubeSat [37] which was successfully launched in December 2015. Subsequent demonstration confirmed its status as a space-capable non-classical light source [32].

5.2 SPEQS-1

A polarisation-entangled version of SPEQS (SPEQS-1) is currently being developed. It will be hosted by a dedicated CubeSat (SpooQy-1) being built at CQT and targeted for launch around the end of 2017. The key challenge upgrading from SPEQS-CS to SPEQS-1 is optical alignment. To achieve polarisation entanglement a greater number of crystals are required and their alignment tolerances (approximately 100 μrad) are more demanding.

5.3 SPEQS-2

While the SPEQS-1 sources demonstrate the entangled pair production and validation principles in orbit, the 2nd generation devices (SPEQS-2) are being developed to increase the production rate of entangled pairs. The new sources should be sufficiently bright for use in space-to-ground QKD [7]. The target performance specifications are shown in Table 3 and the optical layouts in Figure 4.
Figure 4

SPEQS-2 optical layout. SPEQS-1 omits the components marked with square red dots, SPEQS-CS additionally omits the components marked with circular blue dots.

Table 3

SPEQS-CS specifications (GomX-2 version) and design envelopes for upcoming devices

















Power (peak)

2.5 W

2.5 W

10 W


0.3 kg

0.8 kg

1 kg





Brightness refers to the number of detected photon pairs per second per milliwatt. Visibility is a measure of the quality of the photon pairs produced and efficiency refers to percentage of coincident pairs to single photons detected.

Key challenges for the SPEQS-2 development include increasing the APD detection rate to 5 million spontaneous counts per second, managing the extra heat produced by the more powerful pump laser and faster detectors, and keeping the increased number of optical components in alignment [38]. The SPEQS-2 instrument is planned to be launched on the SpooQy-2 spacecraft.

The nominal SpooQySat [39] design is shown in Figure 5 and will be 3U CubeSat with body mounted solar panels, largely-based on the GomSpace GomX platform.
Figure 5

CAD rendering of SpooQy-2 design (with most of the solar panels removed). The green blocks represent the volumes allocated to two SPEQS-2 payloads, allowing redundancy or two design variants of SPEQS to be tested.

If deployed into orbit from the ISS (400 km altitude, 51.65 degree inclination) we estimate it to be able to perform about 90 minutes of SPEQS-2 experiments per day. This could be increased if we use more than just one ground station to downlink the data but is more fundamentally limited by the power generation capabilities of the solar cells (about 6 Wh per day). A 3U CubeSat in an ISS orbit may have a lifetime of 6-12 months before its orbit degrades; other, longer orbital lifetime options are being investigated.

6 Outlook and conclusions

The first practical QKD tests using our SPEQS sources will require measuring one of the photons in the pair on the satellite and beaming the other of the pair down to an optical receiver on Earth or on another satellite. This is a considerably more complex challenge than the current SpooQySat missions. Encouragingly, the technologies for this to be achieved are already existing or in development. Such technologies include high precision satellite position knowledge through GNSS (Global Navigation Satellite System) and laser ranging, high precision ADCS (Attitude Determination and Control Subsystem) [40], optical beam steering [41], transmission optics [42] and optical ground stations [43]. CubeSats have already been built for conventional laser communications [44] and advanced platforms that might one day enable this at the single-photon level are also under development [45].

The rapid progress in experimental quantum optics over the past two decades has been possible because the financial barrier to participation in the scientific work has been modest. As quantum technology matures and its deployment into novel environments begin to take place, the rate of innovation and experimentation may begin to slow down if the financial costs make participation difficult.

Nanosatellite platforms may be key to getting space access for a larger number of university groups, and this in turn, will spur work on getting experiments ready for small spacecraft. We believe the quantum technology community who are interested in space missions cannot afford to overlook the potential of nanosatellites.



The Singapore-based team is supported by the Singapore National Research Foundation under its Competitive Research Programme (CRP12-2013-02). D. Oi acknowledges the Scottish Quantum Information Network (QUISCO) and the EU FP7 CONNECT2SEA project “Development of Quantum Technologies for Space Applications”.

Open Access This article is distributed under the terms of the Creative Commons Attribution 4.0 International License (, which permits unrestricted use, distribution, and reproduction in any medium, provided you give appropriate credit to the original author(s) and the source, provide a link to the Creative Commons license, and indicate if changes were made.

Authors’ Affiliations

Centre for Quantum Technology, National University of Singapore
SUPA Department of Physics, University of Strathclyde
Department of Physics, National University of Singapore


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