Space and Exploration Technology
The Space and Exploration Technology Group (SET) delivers frontier research across access to space, in-orbit and planetary exploration technologies, including underpinning work on orbital dynamics and mission design. Through simulation, laboratory-scale demonstration and terrestrial analogues, our work is developing key technologies to enable the exploration missions and satellite applications of the future. Our laboratory-based research activities are centred on the Integrated Space and Exploration Technologies Laboratory (I-SET), recently up-graded to provide an air-bearing and Helmholtz coil, vacuum chamber, clean room area and 3D printing facilities. A new European Space Agency (ESA) funded space environment chamber will support work on rocket plume-regolith interaction for lunar, Mars and asteroid missions.
Our staff
Academic staff |
Research Assistants |
PhD candidates |
|---|---|---|
| Prof Colin McInnes | Dr Gilles Bailet | . |
| Prof Konstantinos Kontis | Dr James Beeley | Krzysztof Bzdyk |
| Prof Patrick G Harkness | Dr Onur Celik | . |
| Dr Matteo Ceriotti | Dr Litesh Sulbhewar | Livia Ionescu |
| Dr Kevin Worrall | Dr Iain Moore | . |
| Dr Andrea Cammarano | Satyam Bhatti | Robbie Gordon |
| Dr Hossein Zare-Behtash | Vaibhav Somaji Anuse | Dorota Budzyn |
| Dr Mohammad Yazdani-Asrami | Khaldon Al-Areqi | Luca Löttgen |
| Andrew Scott-George | Christopher Teale | |
| Majid Alhajeri | ||
| Jack Tufft | ||
| Zitong Lin | ||
| Claudia Jimenez Cuesta | ||
| Matthew Deans | ||
| Edward Tomanek-Volynets | ||
| Jack Davies | ||
| Abdullah Akdogan |
Access to space
Patrick Harkness, Konstantinos Kontis, Kevin Worrall
Small satellites are typically launched on large vehicles, but there are constraints on cost and orbits which can be accessed.
Our solution
Hypersonic re-useable vehicles - or burn rocket casing as fuel, enabling nano-launchers sized for individual small satellites.
We are developing the autophage launch vehicle in collaboration with Dnipro National University. This concept is a rocket which consumes its own structure for propellant during ascent, thereby reducing the dry mass of the vehicle to a near-zero value. The result is that the launch vehicle can be scaled down such that it is matched to an individual nanosat.
Our partners
Dnipro National University, Orbital Access Ltd (Prestwick)
Space technologies
Colin McInnes, Kevin Worrall, Matteo Ceriotti
New technologies are required to unlock and underpin the commercial satellite applications of the future.
Our solution
Though a Royal Academy of Engineering Chair in Emerging Technologies we are investigating new concepts for space technologies, satellite platforms and mission design from micro-to-macro length-scales. By pushing the boundaries of length-scale to these extremes, it is anticipated that unsuspected new concepts will emerge which can underpin the new downstream satellite applications of the future. Our work is delivering a mix of modelling and simulation, laboratory-scale bread-boarding and ultimately in-orbit demonstration as appropriate. For example, our PCB-satellite programme is developing a 3x3 cm device with 3-axis attitude control, while our work on in-orbit fabrication is investigating direct printing of structural materials onto membranes in vacuum.
Micro-scale: We envisage a new class of space system delivering real-time, high spatial resolution measurements of the space environment using massively parallel sensing with clouds of networked sensor nodes. Services could include space weather monitoring through MEMs-scale magnetometers embedded in each node, or support for large platforms through visual inspection and fault detection.
Meso-scale: Future platforms can be configured using 2D arrays of unfolding planar modules, each hosting computing, power and communications. By reconfiguring the geometry of such arrays, adaptable platforms can be envisaged which can be reconfigured to deliver a range of mission applications, while their time-varying inertia matrix enables new and novel attitude control strategies.
Macro-scale: By directly printing structures onto thin film reflective membranes, ultra-large gossamer reflectors can be fabricated in-orbit. We envisage new energy services with sunlight reflected onto large terrestrial solar PV farms at dawn/dusk when spot prices are high. Other applications include thermal power for in-orbit manufacturing, potentially to process near Earth asteroid resources.
Other work includes micro-satellite attitude control with Alba Orbital Ltd, supported through a Royal Academy of Engineering Industrial Fellowship, and work on machine learning with Craft Prospect Ltd.
Our partners
Royal Academy of Engineering, Alba Orbital Ltd, Craft Prospect Ltd
Orbital dynamics
Matteo Ceriotti, Colin McInnes
Once in space, spacecraft require efficient orbit manoeuvres to deliver mission objectives, and reach new orbit and vantage points and orbits.
Our solution
We explore the dynamics of multi-body gravitational interactions and non-gravitational perturbations in order to design new families of efficient spacecraft trajectories. This includes work on new methodologies for trajectory optimisation and the use of light pressure for solar sailing to deliver new families of highly non-Keplerian orbits which can enable entirely new vantage points in space.
Through new insights into asteroid orbital dynamics we are leveraging multi-body gravitational interactions to reduce the scale of engineering required for asteroid capture, part supported by a Royal Society Wolfson Research Merit Award. This includes the use of stable invariant manifolds, aerocapture and kinetic impacts. Other work is investigating energy-efficient asteroid dis-assembly using the ‘orbital siphon’ effect and the interaction of economic models with trajectory optimisation and mission design.
We exploit Deep Learning and Artificial Neural Networks to quickly identify feasible and low-cost trajectories to selected targets among thousands of asteroids. Other research explores the use of new and potentially disruptive space propulsion technologies for future applications. Examples are the use of solar radiation pressure and hybrid propulsion. Applications include the design and control of asteroid proximity orbits using a solar sail. Work on efficient solar sail trajectories is supported through a Marie Skłodowska-Curie Incoming International Fellowship.
Our partners
The Royal Society, EU Horizon 2020 Framework Programme, Clyde Space Ltd
Landing on other worlds
Konstantinos Kontis, Hossein Zare-Behtash, Andrea Cammarano
During atmospheric entry any object from outer space, experiences high temperatures and forces caused by the aerodynamic drag. Dealing with such extreme conditions is challenging and crucial to ensure safe entry for future missions.
In addition, lading on celestial bodies brings further complications due to the presence of regolith – un-weathered highly abrasive and electro-statically charged dust particles that cause a wide range of problems (i.e. clogging, abrasion).
Our solution
In support of planetary and lunar landing environments, we offer a unique set of tools and expertise capable of simulating the re-entry and the conditions faced by the spacecraft during descend and landing. The University of Glasgow hosts a large volume dirty vacuum facility capable of achieving and maintaining high vacuum conditions even when the additional mass flow such as that encountered during jet firing.
By adopting a synergetic approach involving advanced experimental measurements (e.g. PIV, Schlieren, IR Thermography) and numerical tools (rarefied gas modelling, optimal sensing network design and physics informed neural network), we investigate fundamental problems to devise industry pertinent solutions to ongoing challenges.
Our partners
ESA-ESTEC, NASA, OHB, Astronika, ESA-EAC, ESA-SACF.
Our facilities
Surface and subsurface exploration
Patrick Harkness, Colin McInnes, Kevin Worrall, Matteo Ceriotti
Drilling in low gravity (asteroids, Moon and Mars) with no real-time control requires new exploration technologies.
Our solution
Exploration activities focus on the penetration of granular, rocky, and permafrost/ice materials. We have demonstrated that granular materials can be fluidised by ultrasonic excitation, and this facilitates penetration across a wide range of apparent gravities. Ultrasonic and percussive techniques have been used to penetrate and core-sample rock, and technology transfer activities have spun these concepts out into subglacial polar exploration on Earth. All these systems have been supported by robotic systems, and we have demonstrated drill-assembly and disassembly for space, as well as larger subterranean tunnelling robotic concepts for use on Earth. We also investigate the extraction of asteroid resources for utilisation in space.
Our partners
British Antarctic Survey, EU H2020 (biomimetic tunneling robot)
We engage heavily in field deployment of our hardware, including to sites in Tenerife, Boulby Underground Laboratory, and Antarctica; as well as to other labs in places such as Aachen, ESTEC and Dnipro.
