OPS-SAT

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OPS-SAT [1]
Tiny sat, big ambitions ESA376721.jpg
Engineering model of OPS-SAT, seen on a test bench
Mission typeTechnological demonstrator
Operator ESA
SATCAT no. 44878 OOjs UI icon edit-ltr-progressive.svg
Website www.esa.int/Our_Activities/Operations/OPS-SAT
Spacecraft properties
Bus 3U CubeSat
Manufacturer Graz University of Technology, Austria
Launch mass7 kg
Dimensions96 mm × 96 mm × 290 mm
(3.8 in × 3.8 in × 11.4 in)
Start of mission
Launch date18 December 2019
Rocket Soyuz VS23 [2] · [3]
Launch site Centre Spatial Guyanais
( Ensemble de Lancement Soyouz )
Contractor Arianespace [4] · [5]
 

OPS-SAT is a CubeSat by the European Space Agency (ESA) and it is intended to demonstrate the improvements in mission control capabilities that will arise when satellites can fly more powerful on-board computers. The mission has the objective to break the cycle of "has never flown, will never fly" in the area of satellite control. It was the first CubeSat operated directly by ESA. [1]

Contents

The satellite has an experimental computer that is ten times more powerful than traditional ESA on-board computers. This on-board computer provides an experimental platform to run software experiments on board. One innovative concept is the deployment of space software in the form of apps. This concept is enabled by the NanoSat MO Framework (NMF) and allows Apps to be uploaded to the spacecraft and then started on board. This is a new concept that ESA has successfully demonstrated in space. [6]

OPS-SAT has been launched at 08:54:20 UTC on 18 December 2019 exactly twenty-four hours later than originally planned.

Payload and communications

OPS-SAT will provide an in-orbit test-bed environment for the deployment of different experiments to test new protocols, new algorithms, and new techniques. The satellite is being designed to be robust and no single point of failure should exist, therefore it shall be always possible to recover the spacecraft if something goes wrong with one of the software experiments. The robustness of the basic satellite itself will allow ESA flight control teams to upload and try out new, innovative control software submitted by experimenters.

OPS-SAT payload devices:

Communication links to ground:

Experimental Platform

The Experimental Platform of OPS-SAT is where experiments will be running. It has two Critical Link MityARM 5CSX in cold redundancy (if one fails, the second one is used). These have a Dual-core 800 MHz ARM Cortex-A9 processor, an Altera Cyclone V FPGA, 1 GB DDR3 RAM, and an external mass memory device with 8 GB. [7]

ESA's aim is to remove as many barriers to experimentation as possible. For example, there will be no paperwork, ESOC's infrastructure will be ready to do automated tests on the experiments, and aims at reducing the overheads close to zero. Additionally, the experiments can be easily developed in form of apps using the NanoSat MO Framework.

Awards

In March 2023, the OPS-SAT Mission Control Team was awarded with the International SpaceOps 2023 Award for Outstanding Achievement. [8]

OPS-SAT's Firsts

OPS-SAT has achieved several significant firsts in various areas. [9]

Operations

Artificial Intelligence

Protocols and Standards

Cybersecurity

Noteworthy

NanoSat MO Framework (NMF)

The most innovative concept in OPS-SAT is the deployment of space software in the form of apps. The European Space Agency in collaboration with Graz University of Technology investigated and developed the NanoSat MO Framework. [28]

The NanoSat MO Framework (NMF) is a software framework for nanosatellites based on CCSDS Mission Operations services. It includes a Software Development Kit (SDK) to develop experiments as NMF Apps which can then be installed, started, and stopped in space. The framework also includes monitoring and control capabilities for the apps which will allow experimenters from the ground to take control of their software when it is running in space. [29]

The OPS-SAT system image comes with the NanoSat MO Framework which interfaces with all of the OPS-SAT payload systems and provides it in the form of services to the experimenter application. The NanoSat MO Framework allows simple integration of other libraries and applications. During the development of the experiments, the NMF SDK can be used and it includes a simulator, providing most of the platform functionalities accessible to the experimenter. The simulator allows developers to make their NMF Apps without the need to access an advanced satellite testbed hardware platform.

On the ground, EUD4MO will provide a web-based solution for the monitoring and control of NMF Apps. OPS-SAT experimenters will be able to take control using their web browser.

See also

Related Research Articles

<span class="mw-page-title-main">European Space Operations Centre</span> Main mission control centre for the European Space Agency

The European Space Operations Centre (ESOC) serves as the main mission control centre for the European Space Agency (ESA) and is located in Darmstadt, Germany. ESOC's primary function is the operation of uncrewed spacecraft on behalf of ESA and the launch and early orbit phases (LEOP) of ESA and third-party missions. The Centre is also responsible for a range of operations-related activities within ESA and in cooperation with ESA's industry and international partners, including ground systems engineering, software development, flight dynamics and navigation, development of mission control tools and techniques and space debris studies.

<span class="mw-page-title-main">CubeSat</span> Miniature satellite in 10 cm cube modules

A CubeSat is a class of small satellite with a form factor of 10 cm (3.9 in) cubes. CubeSats have a mass of no more than 2 kg (4.4 lb) per unit, and often use commercial off-the-shelf (COTS) components for their electronics and structure. CubeSats are deployed into orbit from the International Space Station, or launched as secondary payloads on a launch vehicle. As of December 2023, more than 2,300 CubeSats have been launched.

<span class="mw-page-title-main">Interplanetary Internet</span> Model of Internet between planets

The interplanetary Internet is a conceived computer network in space, consisting of a set of network nodes that can communicate with each other. These nodes are the planet's orbiters and landers, and the Earth ground stations. For example, the orbiters collect the scientific data from the Curiosity rover on Mars through near-Mars communication links, transmit the data to Earth through direct links from the Mars orbiters to the Earth ground stations, and finally the data routed through Earth's internal internet.

The Satellite Control and Operation System 2000 (SCOS-2000) is the generic satellite Mission Control System (MCS) software infrastructure developed and maintained by the European Space Agency (ESA/ESOC) in collaboration with European industry and deployed for missions such as Radarsat 2, XMM-Newton, INTEGRAL, Cryosat, Mars Express, Venus Express, GOCE, Herschel, Planck, Rosetta, Cryosat-2, Galileo, MetOp, LISA Pathfinder, SWARM, Gaia, SENTINEL spacecraft, EXOMARS orbiters, METEOSAT Third Generation, Aeolus, BepiColombo, SOLO or EUCLID. Upcoming missions that will deploy SCOS-2000 include MetOp-SG and EarthCARE.

The Spacecraft Monitoring & Control (SM&C) Working Group of the Consultative Committee for Space Data Systems (CCSDS), which sees the active participation of the main space agencies, is defining a service-oriented architecture consisting of a set of standard end-to-end services between functions resident on board a spacecraft or based on the ground, that are responsible for mission operations.

The Nano-Japan Astrometry Satellite Mission for Infrared Exploration (Nano-JASMINE) is an astrometric microsatellite developed by the National Astronomical Observatory of Japan, with contributions by the University of Tokyo's Intelligent Space Systems Laboratory (ISSL). As of 2015, the satellite was planned for launch together with CHEOPS in 2019. However, this launch took place in December 2019 without Nano-JASMINE as one of the three piggyback payloads. Some sources named 2022 as the launch year of the satellite.

The Global Educational Network for Satellite Operations (GENSO) is forming by a worldwide network of ground stations and spacecraft which can interact via a software standard. The GENSO aims to increase the return from educational space missions and changed the way that these missions are managed, dramatically increasing the level of access to orbital educational spacecraft.

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<span class="mw-page-title-main">CHEOPS</span> Optical space telescope (launched in 2019)

CHEOPS is a European space telescope. Its objective is to determine the size of known extrasolar planets, which will allow the estimation of their mass, density, composition and their formation. Launched on 18 December 2019, it is the first Small-class mission in ESA's Cosmic Vision science programme.

<span class="mw-page-title-main">Nanoracks</span> Private space hardware and services company

Nanoracks LLC is a private in-space services company which builds space hardware and in-space repurposing tools. The company also facilitates experiments and launches of CubeSats to Low Earth Orbit.

The Spacecraft Monitoring & Control (SM&C) Working Group of the Consultative Committee for Space Data Systems, which sees the active participation of 10 space agencies and of the Space Domain Task Force of the Object Management Group, is defining a service oriented architecture consisting of a set of standard end-to-end services between functions resident on board a spacecraft or based on the ground, that are responsible for mission operations.

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<span class="mw-page-title-main">Nanosat 01</span>

The Nanosat 01, sometimes written as NanoSat-1 or NanoSat 01, was an artificial satellite developed by the Spanish Instituto Nacional de Técnica Aeroespacial (INTA) and launched 18 December 2004. Considered a nano satellite for its weight of less than 20 kg, its main mission was forwarding communications between far reaching points of the Earth such as Juan Carlos I Antarctic Base from mainland Spain. This was possible due to its polar orbit and altitude of 650 km above sea level. During an operational run the data obtained in the Antarctic would be uploaded to the satellite during its fly by and then, downloaded in Spain when satellite reached the Iberian Peninsula.

<span class="mw-page-title-main">SpaceX CRS-23</span> 2021 American resupply spaceflight to the ISS

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<span class="mw-page-title-main">LICIACube</span> ASI CubeSat aboard DART spacecraft

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Phi-Sat-2 is an Earth observation CubeSat mission from the European Space Agency (ESA) platform capable of running AI apps directly on board. What makes Phi-Sat-2 particularly noteworthy is its utilization of the NanoSat MO Framework, a modular and open-source platform designed for small satellite missions.

<i>Hera</i> (space mission) ESA spacecraft which will study the effects of the DART Impactor on the asteroid moon Dimorphos

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References

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  5. CHEOPS - Mission Status & Summary
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