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Aerodynamics and flight mechanics
Detonics
Internal ballistics
Laser sources and their applications
High pulsed power technology
Protection and perforation
Optronics and sensors
Protection of military personnel
Homeland Security
Free-Flight Investigations
Precision-Guided Flying Vehicles
Investigations in Aerodynamics
Nanoenergetics
Nanocarbonaceous Materials with Energetic Techniques
Opto-Pyrotechnical Technology
Spectroscopy - A Helpful Instrument
High-Voltage Marx Generators
Semiconductor Technology
Electromagnetic Railgun
High-Power Semiconductor Switches – Multichip Thyristor
High-Power Microwave Metrology
Image Change Detection for IED Detection
Protection of Military Personnel against Noise and Blast Waves
Night Vision for Security
Laser Neutralization of Explosive Devices
Acoustic Detection and Localization
Countering the Threat from IEDs
Illicit Substance Detection with NQR
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High pulsed power techn ...
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Electromagnetic Railgun
FRANCAIS
DEUTSCH
Aerodynamics and flight mechanics
Detonics
Internal ballistics
Laser sources and their applications
High pulsed power technology
> High-Voltage Marx Generators
> Semiconductor Technology
> Electromagnetic Railgun
> High-Power Semiconductor Switches – Multichip Thyristor
> High-Power Microwave Metrology
Protection and perforation
Optronics and sensors
Protection of military personnel
Homeland Security
Electromagnetic Railgun
Purpose
Development of reliable sliding electric contacts at high current densities
Medium-term applications: RApid FIre RAilgun (RAFIRA)
Optimization of payload acceleration using high-end composite materials
Innovative Segmented Railgun
SR/3-60
Concepts for launch to space.
Projectile for SR/3-60
Skills
Physics of high-power railguns
Pulsed power technology for railguns
Innovative metrology (e. g. Doppler radar and CMR sensors)
Dynamical mechanical processes.
Facilities
PEGASUS (cal.: 40 mm, length: 6 m) with
10 MJ for payload ~acceleration
RAFIRA (cal.: 25 mm, length: 3 m) with
2.7 MJ for air defence
SR/3-60 (Ø 28 mm, 3 segmented stages at 0.7 m) with 0.5 MJ.
Results
Hypervelocity: projectiles with 300 g up to
2.5 km/s
Multishot projectiles with 100 g up
to 2 km/s (1.8 km/s with low rail erosion)
Proof of concept for space launch
(PEGASUS): 4 kg up to 500 m/s
Highly local measurements of strong
transient magnetic fields using CMR sensors.
X-ray of the separating sabot
(ISL-patent) during launch inside
the railgun
RAFIRA (v
O
> 1300 m/s, cadence > 20 Hz)
PEGASUS, electromagnetic launch of nanosatellites
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