Projekty českých univerzitních pracovišť

ČESKÉ VYSOKÉ UČENÍ TECHNICKÉ PRAHA
Fakulta elektrotechnická, katedra měření

vedoucí katedry prof. Ing. Pavel Ripka, CSc. 

1. Development and construction of tri-axial vector fluxgate magnetometer for Czech satellite MIMOSA.

2. Development of physical sensor simulator for MAC04 micro-accelerometer (SWARM mission).

3. Continuous development of high precise fluxgate magnetometers (compassing, military – bomb detection, medical applications), development of miniature PCB fluxgate sensors.

4. Calibration of magnetometers (non-magnetic calibration platform for scalar calibration of magnetometers and accelerometers – in cooperation with DTU SPACE, Denmark)

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ČESKÉ VYSOKÉ UČENÍ TECHNICKÉ PRAHA
Fakulta strojní, Ústav letadlové techniky

vedoucí ústavu  doc.Ing. Luboš Janko, CSc. 

Study program:
Aerospace Engineering (Mgr.), courses: Aircraft Design, Aircraft Engines Design
Orientation and Current Projects: Safety and performance of light aircrafts (VLA),
Aircraft design in category of sport and light aircrafts,
External and Internal aerodynamics applications,
3D Flow Fields Investigation in Aeronautical Applications,
Flight Mechanics applications,
Structural Strength and Fatigue Life Tests,
Airplane Structural Life Monitoring,
Modal analysis and Ground Vibration (Flutter) Tests,
Composite materials and structures in VLA category,
Ultra-Lightweight Ducted Fan Propulsion Unit

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ČESKÉ VYSOKÉ UČENÍ TECHNICKÉ PRAHA
Fakulta elektrotechnická, katedra řídicí techniky

vedoucí katedry prof.Ing. Michael Šebek, DrSc.

Program
Space Master  

VYSOKÉ UČENÍ TECHNICKÉ BRNO
Fakulta elektrotechniky a komunikačních technologií, Ústav radioelektroniky

vedoucí ústavu Prof.Dr.Ing. Zbyněk Raida
prof. Ing. Miroslav Kasal, CSc., vedoucí Laboratoře experimentálních družic

Experimental Satellites Laboratory - Advanced research and development result description:

1. Satellite Phase 3D - Two L-band receivers have been developed for this satellite in ESL. The first one is main command receiver and second one is a part of matrix transponder. This work was successfully finalized in the year 2000.

2. Satellite telemetry and command station - Development of basic equipment for the telemetry gathering and command station IREL BUT has been finalized at Brno University of Technology in 2003. The arrangement is suitable for the satellite on high elliptical (HEO) and low Earth (LEO) orbits. The equipment consists of antennae system for automatic satelite tracking, collection of receivers and transmitters, low noise amplifiers, down and up frequency converters, rf power amplifiers, modems and terminal node controllers.

3. PCSAT2 project - Transponder for narrow band and multi-user data communication with extremely high spectral effectiveness. Main goal of the project was to verify possibilities of keyboard-tokeyboard satellite communication. The whole appliance passed all pre-flight tests and was delivered to the International Space Station ISS in 2005 and one year tested. We have got the receiver back to our laboratory for investigation of a space environment influence after end of the mission .

4. Satellite Phase 3E - Project of Phase 3E experimental satellite. The satellite is planned to be on HEO orbit as well, with 60o inclination. It will be smaller in size comparing to Phase 3D satellite and its main function will be to verifycommanding and ranging in extreme conditions, i.e. to verify our developed technologies for next satellite mission P5A to Mars. 

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Česká kosmická kancelář
Centrum studentských aktivit
Kateřinská 10, 128 00 Praha 2
Milan Halousek, e-mail: halousek@czechspace.cz
tel.:  602 153 564