European Student Moon Orbiter

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The European Student Moon Orbiter (ESMO) was a proposed European student mission to the Moon. Student teams from 19 universities throughout Europe worked on the program. ESMO was conceived by the Student Space Exploration & Technology Initiative (SSETI) under the support of the European Space Agency (ESA); prior to the start of Phase A the full responsibility for the management of the program was transferred to the ESA Education Office.

Contents

In 2009, Surrey Satellite Technology Ltd (SSTL) was selected as prime contractor. [1] In April 2012, ESMO was scheduled for launch in 2014 or 2015, [1] but further ESA evaluation deemed the ESMO project's costs "unsustainable" given the ESA Education Office's budget. [2]

Objectives

The mission objectives for ESMO were: [3]

The educational aim of the project was to provide valuable hands-on experience to university students within a real and demanding space project. This is in order to fully prepare a well qualified workforce for ambitious future ESA missions. [3]

Lunar transfer

The spacecraft of approximately 190 kg (420 lb) mass and a size of 76 × 74 × 74 cm (30 × 29 × 29 in) was designed to be launched as a secondary or auxiliary payload into Geostationary transfer orbit (GTO) in 2014/2015. From there, the spacecraft would use its on-board propulsion to travel to lunar orbit via a weak stability boundary transfer. This travel via the Sun-Earth L1 Lagrange point would take three months, but it requires much less propellant than a direct transfer (see Low energy transfer [4] [5] and Interplanetary Transport Network). [1] [3] ESMO is intended to be operated in lunar orbit for six months.

Payloads

Payloads that were considered for the orbiter included: [3]

Technical facts

The table below provides an overview of the planned spacecraft platform and the ground segment. [3]

SubsystemDescription
Attitude Determination and Control System (ADCS)3-axis stabilized: 2 star trackers, 4 Sun sensors, 2 inertial measurement units, 4 reaction wheels, 8 cold gas thrusters
On-board Data Handling2 ESA LEON2 processors (dual redundant) running data handling software (command timeline and simple FDIR) and ADCS software; 32 MB Serial Flash for payload data storage; CANbus data interfaces
CommunicationsLow Gain Antennas for omni-directional coverage; S-band transponder with PSK-PM modulation and range and range rate capability for radio-navigation; 8 kbit/s downlink / 4 kbit/s uplink between Moon and Earth stations
PowerBody-mounted 3J GaAs solar cells for 170 W beginning of life power and 122 W end of life power; 24-29 V unregulated bus; 1800 Wh capacity Li-ion batteries
Propulsion4 liquid MON/MMH bipropellant thrusters: 22 N thrust each, 285 s specific impulse (modulated by AOCS software during burns for reaction control)
StructureCFRP/Al honeycomb construction box with load bearing central thrust tube
Thermal ControlPassive: MLI and surface coatings; active: local heaters for eclipse (e.g. propellant tanks)
Ground SegmentGround stations: 25m S-band dish in Raisting and 15m S-band dish in Villafranca; Perth/Kourou for launch and early orbit phase and manoeuvres

Participating teams

Twenty-one teams from 19 European universities in ESA member states and cooperating states were part of the project.

UniversityCountryResponsibilities
University of Liège BelgiumNarrow Angle Camera Payload
Czech Technical University in Prague Czech RepublicAOCS Interface Module
University of Tartu EstoniaAssembly, Integration and Verification and Satellite Operation
Supaero FranceStar Tracker
University of Stuttgart GermanyPropulsion System - Gas Feed (Cold Gas Thruster)
Technische Universität München GermanyLunaNet Payload & Ground Station
University of L'Aquila and University of Rome La Sapienza ItalyMicrowave Radiometer Scientific Payload
Politecnico di Milano ItalyAttitude Determination and Control System
Politecnico di Milano ItalyPropulsion System - Liquid Feed (Bipropellant Thruster)
Warsaw University of Technology PolandThermal Control Subsystem
Wroclaw University of Technology PolandCommunications System
AGH University of Science and Technology PolandSpace Environment & Effects Analysis
Politehnica University of Bucharest RomaniaAttitude Determination and Control System
Politehnica University of Bucharest RomaniaStructure
University of Bucharest RomaniaRadiation Monitor Payload
University of Ljubljana SloveniaSimulator
University of Ljubljana SloveniaRadar Payload
University of Maribor SloveniaOn-board Data Handling
University of Oviedo SpainHarness
University of Vigo SpainGS/OPS-V team. Ground Station VIL-1 team.
University of Glasgow United KingdomMission Analysis and Flight Dynamics
University of Southampton United KingdomSystem Engineering
University of Warwick United KingdomPower Subsystem

Led by ESA's Education Office at ESTEC, the project successfully completed a Phase A feasibility study and continued with the preliminary design during Phase B. More than 200 students were involved in Phases A and B of the ESMO project. Since November 2009, SSTL coordinated and supervised the work of the students, providing system-level and specialist technical support. Regular workshops at ESTEC and ESOC as well as internships at SSTL were organized to support the student teams in their ESMO related activities and provide training / knowledge transfer. Additionally, facilities at SSTL were to be utilized for spacecraft assembly, integration and testing. As a major milestone during Phase B, the System Requirements Review (SRR) for ESMO was performed in 2010. At SRR, the system requirements and system design were finalised. Part of the SRR also selected the university teams to participate in the following phases of the project. After passing a preliminary design review in March 2012, the program was ended as a result of budget constraints in April 2012. ESMO was to have been the fourth mission within ESA's Education Satellite Programme following SSETI Express, YES2 and the European Student Earth Orbiter (ESEO). [3]

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References

  1. 1 2 3 "Development of the ESMO student Moon satellite gets under way / Education / ESA". ESA. Retrieved 13 April 2013.
  2. "ESA concludes student ESMO Moon orbiter project".
  3. 1 2 3 4 5 6 "ESMO mission / Education / ESA". ESA. Retrieved 13 April 2013.
  4. Zuiani F., Gibbings A., Vetrisano M., Rizzi F., Martinez C., Vasile M.. Orbit Determination and Control for the European Student Moon Orbiter. Acta Astronautica, 2012, 79. pp. 67-78. ISSN 0094-5765
  5. Vetrisano M., Van der Weg W., Vasile M., Navigating to the Moon Along Low-Energy Transfers, Celestial Mechanics and Dynamical Astronomy, 2012, October 2012, Volume 114, Issue 1-2, pp. 25-53