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![Page 1: Presentazione di PowerPoint - UNISEC-Global · Presentazione di PowerPoint Author - - Created Date: 7/5/2015 2:17:57 AM](https://reader034.vdocuments.mx/reader034/viewer/2022042317/5f061b427e708231d4165288/html5/thumbnails/1.jpg)
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Satellite systems design
• Mission analysis
• On-board systems/sub-system
• Ground station operations
• Data handling and processing
MAIN
RESEARCH
ACTIVITIES
Space surveillance systems
• Optical observation systems
• Data analysis
• Orbit determination
• Active debris removal systems
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• It is a functional spacecraft, rather than a payload instrument or component. To fit the definition, the device must operate in space with its own independent means
of communications and command
• Untrained personnel (i.e. students) performed a significant fraction of key design decisions, integration &
testing, and flight operations
• The training of these people was as important as (if not more important) the nominal “mission” of the spacecraft
itself
UNIVERSITY
SATELLITE
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Design
Building
Testing
Operations
CUBESAT
DEVELOPMENT
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DESIGN
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TESTING
1U Cubesat structure vibration test results
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BUILDING
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OPERATIONS
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ON-GOING
SPACE
PROJECTS
Research programs
Education programs & International contests/competitions
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QB50 PROJECT
URSA MAIOR
URSA MAIOR PAYLOADS
1. A de-orbiting system experiment
2. MEMS MicroThruster Experiment
(MEMIT)
QB50 has the scientific objective to
study in situ the temporal and spatial
variations of a number of key
constituents and parameters in the lower
thermosphere (90‐320 km) with a
network of 50 double CubeSats
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EQUOEquatorial Observatory for
Space Debris
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LEO High Inclination tracking from Italy and Kenya (Terminator Shape)
Continuous tracking of LEO objects
from Italy and Kenya
ALMASCOPE: 2010 Equatorial test campaign
• Telescope - 25 cm f/4 in newtonian
configuration
• CCD Kaf1600E sensor , 1024x1536
pixels, each pixel is 9x9 micron (total
chipsize 9.2x13.8 mm)
• Mount German equatorial
• The field of view is of about 1 degree
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IRIDIUMInvestigating Radiation Impact and
Damages In UV-sensitive Materials
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SCIENTIFIC GOAL: analyse material degradation after UV exposure and Investigate damages by synergic effects in the stratosphere environment
TECHNICAL GOAL: develop and test a rotating tubular beam, fastening the samples holder, able to maintain the optimal exposition to sunlight during the BEXUS
flight
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HORUS CASTThe celestial constellation
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HORUS cast combine a nadir-pointing camera
to off-set nadir optical sensors in order to
provide a multiple angle capability for sampling
This architecture scheme is similar to the
MISR sensor (Multi-angle Imaging
SpectroRadiometer), successfully tested on
NASA EOS Terra satellite (total mass 5,190 kg)
The Pre 4th Mission Idea Contest
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CANSAT
competition
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CanSat Competition is an annual student design-build-launch competition for
space-related topics, organized by The American Astronautical Society (AAS)
and American Institute of Aeronautics and Astronautics (AIAA)
Students by S5Lab participate to this competition with the Sapienza Space
Team, supported by SASA Sapienza Aerospace Student Association. The 2015
mission simulates a Science Vehicle traveling through a planetary atmosphere
sampling the atmospheric composition during descent.
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LABORATORY
FACILITIES
Laboratory low-vacuum chamber
Electronics development facilityLaboratory milling machine
Workshop
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S5Lab Team
PhD students:
MSc and BSc students:
Federica Angeletti
Quirino Bellini
Salvatore Buonomo
Saverio Cambioni
Andrea Chiovini
Federico Curianò
Michele Gaeta
Alessandro Gallo
Armando Grossi
Paolo Marzioli
Paolo Panicucci
Alice Pellegrino
Tullio Petruzziello
Vito Lamarca
Veronica Vilona
Federica Zaccardi
Giulia Zaccari
Lorenzo Arena
Tommaso Cardona
Francesco Diprima
Gioacchino Scirè
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THANKS FOR
LISTENING!