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CISAS "G.Colombo"
Center of Studies and Activities for Space

HYPERVELOCITY
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General capability
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SOLAR SYSTEM PHYSICS
Mars exploration
Venus exploration
Titano exploration
Mercury exploration
Vesta and Ceres exploration
Rosetta mission
ASTRONOMY & ASTROPHYSICS
Universe observations
Relativistic Astrophysics
Orbital analysis
GEOPHYSICS & GEODESY SPACE
GPS geodesy
Geophysics using GPS
Measure of earthly gravitational field
SPACE SYSTEMS
Rocket
Space propulsions
Hypervelocity
Space robotics
Stratospheric flight
SPACE PSICOLOGY
Cardiac Rhythm of spaceman
STRATEGY AND SPACE ORGANIZATION
Management of space projects
Thecnologic research
TECHNOLOGY TRANSFER
Collaboration with small enterprises
Industrial Innovation
Collaboration with other institutions
ENGINEERING CLINICAL
Isolated Perfused Liver
SERVICES
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Publication and Preprints
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Hypervelocity facility description
CISAS Hypervelocity Impact Facility is based upon a two-stage Light-Gas Gun (LGG), that can achieve a very high shot-repetition-rate (up to 10 shots per day) together with low operational costs.

CISAS LGG can launch both solid cylinders and sabots at a maximum velocity of 6 km/s. Sabots are separated by means of aerodynamic drag in the flight chamber and can carry projectiles in the diameter range 0.4 - 3 mm.


LGG MAIN PERFORMANCE
Speed range
Projectile mass

Shot frequency
Barrel diameter
Barrel length
0.3 - 6.0 km/s
150 mg @ 6 km/s
500 g @ 300 m/s
up to 10 shots/day
4.76 or 6 mm
1.5 - 2.5 m
click on the figure to see the animation

The opportunity of performing many tests in a single working day makes it possible to partially overcome one of the limitations in the field of hypervelocity impact testing, i.e. the lack of experiments. The special LGG set-up does not use components that are destroyed during gun operations: high-pressure helium is used instead of powder as piston driver, special automatic valves have been designed to replace rupture disks between the pump tube and the barrel, and the piston extrusion in the pump tube high pressure section is avoided.

The gun has been designed to be a very flexible system to be applied on different problems, from low speed to hypervelocity. It can be used in a single-stage mode (500 grams accelerated up to 300 m/s) and in a two-stage mode (100 mg up to 5.5 km/s).

The gun can launch saboted projectiles allowing the acceleration of particles having different shape and size.

Speed measurement equipment:
The sabot and projectile velocity is measured by recording the time distance between two subsequent break-ups of two laser blades crossing the flight path. A third signal comes up from a photodetector that is sensitive to the light emitted during the impact. The combined use of these methods makes it possible to achieve accuracy below 2% in the velocity measurements.

Photographic equipment
Photographic equipment is available to catch 4 shadowgraphs with a minimum time delay of 1 microsecond between subsequent pictures. This can be used to verify the projectile integrity before the impact or to study the evolution of the debris cloud resulting from the perforation of a target. Three different fields of view are obtainable (80, 110 and 160 mm). The system adopts a trigger that synchronizes automatically the light flashes to the impact, without the need of trial tests.

Acceleration measurement equipment
A measurement system is available to record vibration and deformation signals from different locations on targets. Shock accelerometers (up to 200000 g, resonance frequency 1.2 MHz) can be employed to measure the near-field environment resulting from hypervelocity impacts. Moreover, standard piezoeletric accelerometers and laser vibrometer are available for acceleration measurements in the mid and far-field.
Test
Test on CFRP panels (in collaboration with NAL-JAXA)
Impact experiments in planetary
Test campaign for MPLM (logistic module of ISS)
Spacecraft Disturbances due to Hypervelocity Impact (under ESA contract)
Impact tests on tethers
Tests on ceramic foams

"Purpose of CISAS is to promote, to coordinate and to perform studies and research in space activities which can develop interdisciplinary education and collaboration among Basic Sciences, Applied Research and industrial realisation."