5,379 research outputs found
It's hip to be square : The CubeSat revolution
With the launch of the UK’s first commercial CubeSat, UKube-1, on the horizon, Malcolm Macdonald and Christopher Lowe look at what the future holds for this standardised spacecraft platform
Deploying quantum light sources on nanosatellites II: lessons and perspectives on CubeSat spacecraft
To enable space-based quantum key distribution proposals the Centre for
Quantum Technologies is developing a source of entangled photons ruggedized to
survive deployment in space and greatly miniaturised so that it conforms to the
strict form factor and power requirements of a 1U CubeSat. The Small Photon
Entangling Quantum System is an integrated instrument where the pump, photon
pair source and detectors are combined within a single optical tray and
electronics package that is no larger than 10 cm x 10 cm x 3 cm. This footprint
enables the instrument to be placed onboard nanosatellites or the CubeLab
structure aboard the International Space Station. We will discuss the
challenges and future prospects of CubeSat-based missions.Comment: Submitted to SPIE Quantum Information Science and Technology. Paper
number 9648-4
End to End Satellite Servicing and Space Debris Management
There is growing demand for satellite swarms and constellations for global
positioning, remote sensing and relay communication in higher LEO orbits. This
will result in many obsolete, damaged and abandoned satellites that will remain
on-orbit beyond 25 years. These abandoned satellites and space debris maybe
economically valuable orbital real-estate and resources that can be reused,
repaired or upgraded for future use. Space traffic management is critical to
repair damaged satellites, divert satellites into warehouse orbits and
effectively de-orbit satellites and space debris that are beyond repair and
salvage. Current methods for on-orbit capture, servicing and repair require a
large service satellite. However, by accessing abandoned satellites and space
debris, there is an inherent heightened risk of damage to a servicing
spacecraft. Sending multiple small-robots with each robot specialized in a
specific task is a credible alternative, as the system is simple and
cost-effective and where loss of one or more robots does not end the mission.
In this work, we outline an end to end multirobot system to capture damaged and
abandoned spacecraft for salvaging, repair and for de-orbiting. We analyze the
feasibility of sending multiple, decentralized robots that can work
cooperatively to perform capture of the target satellite as a first step,
followed by crawling onto damage satellites to perform detailed mapping. After
obtaining a detailed map of the satellite, the robots will proceed to either
repair and replace or dismantle components for salvage operations. Finally, the
remaining components will be packaged with a de-orbit device for accelerated
de-orbit.Comment: 13 pages, 10 figures, Space Traffic Management Conference. arXiv
admin note: text overlap with arXiv:1809.02028, arXiv:1809.04459,
arXiv:1901.0971
DISCUS - The Deep Interior Scanning CubeSat mission to a rubble pile near-Earth asteroid
We have performed an initial stage conceptual design study for the Deep
Interior Scanning CubeSat (DISCUS), a tandem 6U CubeSat carrying a bistatic
radar as main payload. DISCUS will be operated either as an independent mission
or accompanying a larger one. It is designed to determine the internal
macroporosity of a 260-600 m diameter Near Earth Asteroid (NEA) from a few
kilometers distance. The main goal will be to achieve a global penetration with
a low-frequency signal as well as to analyze the scattering strength for
various different penetration depths and measurement positions. Moreover, the
measurements will be inverted through a computed radar tomography (CRT)
approach. The scientific data provided by DISCUS would bring more knowledge of
the internal configuration of rubble pile asteroids and their collisional
evolution in the Solar System. It would also advance the design of future
asteroid deflection concepts. We aim at a single-unit (1U) radar design
equipped with a half-wavelength dipole antenna. The radar will utilize a
stepped-frequency modulation technique the baseline of which was developed for
ESA's technology projects GINGER and PIRA. The radar measurements will be used
for CRT and shape reconstruction. The CubeSat will also be equipped with an
optical camera system and laser altimeter to sup- port navigation and shape
reconstruction. We provide the details of the measurement methods to be applied
along with the requirements derived of the known characteristics of rubble pile
asteroids.Comment: Submitted to Advances in Space Researc
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