MAKING SPACE FOR POLAND. Ministry of Economy
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1 MAKING SPACE FOR POLAND Ministry of Economy
2 Relevant Figers for Polish R&D Sector Entities indicating R&D activity 456 Higher Education Schools 1,9 mln of students; Graduates per year; Persons employed in R&D sector; Persons employed in R&D sector have PhD degree PAIiIZ
3 PS Score Points for Publications KH + PS + A Total Score Points Hay Evaluation Factors
4 POLISH SUCCESS RATE in FP7 SPACE
5 Bertin Technologies & Euroconsult Industry Assesement of Poland for Space Activities Instituts B&R Company Telecom & navigation payloads Earth Observation & Science payload Menned Spaceflight hardware Microgravity hardware Satellite Bus Equipment Launcher equipment he EGSE,MGSE simulator On-board processors+software Ground segment network Sat/LV ground station equipment IV&V of on-board software Mission Analysis Satellite ground control software Administration & Support Services Value Added ground system & services Value added system user terminals Mission centres (data archiving) Space related Science and research Maturity level A : Based on previous experience and/or strong synergy with another activity, the entiry has potential to participate in the near term Maturity level B : Based on previous experience in another space or nonspace activity, the entiry may have the potential to participate in the mid term (if the appropriate investment is made) Maturity level C : The entiry has the potential to participate in the long term if the appropriate investment is made
6 The place of R&D ENTITIES in ESA Activity ESA CONTRACTORS BELGIUM (2.69%) FINLAND ( 1.4%) SWITZERLAND ( 2.88%) REGISTRED PARTICIPANTS THIS CONFERENCE ( 2.57%) Total Industry R&D Entities % of R&D
7
8 Polish Science in ESA Programs ISO; ULYSSES; SOHO; CLUSTER; ERS-1,2: Data Interpretation CASSINI/HUYGENS; INTEGRAL; ROSETTA; Space Insrumentation MARS-EXPRESS; VENUS- EXPRES; HERSCHEL/PLANCK;
9 CASSINI / HUYGENS TITAN POLSKA TAM TEŻ BYŁA POLAND WAS HERE SSP THP (Temperature Sensors)
10 R O S E T T A MISSION to COMET POLAND WAS THERE
11 VENUS EXPRESS
12 Space instrumentation Rosetta Herschel Mars-Expresss 12
13 Space Instruments Delivered to ESA Mission last years
14 TECHNOLOGICAL PERFORMANCE Space Instrumentation
15 Scientific Instruments SOLAR X-RAY EXPERIMENTS: 20 instruments delivered by Wrocław Solar Physics Group and launched on 6 rockets and 3 satellites, PLASMA PHYSICS EXPERIMENTS more than 30 instruments Scientific instruments: delivered, 20 satellite missions already completed, another missions in progress, PHYSICAL and GEODESIC STUDIES of PLANETS, EARTH and COMETS: instruments (or subsystems) delivered in 6 missions, a few next in progress, ASTROPHYSICS EXPERIMENTS: IBIS/Integral and HIFI/Herschel
16 AWARDS
17 AWARDS
18 AWARDS
19 MERTIS / BEPI COLOMBO MERTIS Mercury Radiometer and Thermal Infrared Spectrometer Mertis Pointing Unit - MPOI MPOI FM MERTIS FM Electrical Model of MPOI
20 PROBA-3 Coronagraph Polish involvement in the instrument Coronagraph Control Box (CCB) Filter Wheel Assembly, Filters& Polarizes Structure &Baffle
21 Primary Power lines from BNR1 MIU to/from MPU-1 digital interface Supply of internal MPU1 electronics SLOW START & EMC FILTER 40 Programming the overcurrent limits (2 bits x 4 currents x 5 users = 40 I/O pins connected to +5V or to GND) +12V_1-12V_1 +5V_1 +3.3V_1 SEC_0V_1 FPGA STATE MACHINE SPI +12V DC/DC Converter -12V DC/DC Converter +5V DC/DC Converter +3.3V DC/DC Converter CS_ADC1 CS_ADC2 CS_ADC4 CS_ADC3 MIU ON/OFF?? PH-A ON/OFF DE1-A ON/OFF DE2-A ON/OFF XG-A ON/OFF ADC 1 ADC 2 ADC 4 ADC 3 SEC_0V_1 PH-A CURRENTS DE1-A CURRENTS DE2-A CURRENTS MIU-M CURRENTS 4 +12V_1 +12V_AGND_1-12V_1 CURRENT MONITOR. -12V_AGND_1 +5V_1 +12V_1 to MIU-M +5V_GND_1 +3.3V_1 +3.3V_GND_1 4 ON/OFF SWITCHES CURRENT MONITOR. +12V_1 to PH-A ON/OFF SWITCHES CURRENT MONITOR. +12V_1 to DE1-A ON/OFF SWITCHES CURRENT MONITOR. +12V_1 +12V_AGND_1-12V_1-12V_AGND_1 +12V_1 to DE2-A +5V_1 +5V_GND_1 +3.3V_1 +3.3V_GND_1 XG-A CURRENTS 4 +12V_1 VOLTAGE -12V_1 VOLTAGE +5V_1 VOLTAGE +3.3V_1 VOLTAGE MPU1 TEMPERATURE ON/OFF SWITCHES +3.3V_GND_1 +3.3V_1 +5V_GND_1 +5V_1-12V_AGND_1-12V_1 +12V_AGND_1 MIU ON/ OFF?? V_GND_1 +3.3V_1 +5V_GND_1 +5V_1-12V_AGND_1-12V_1 +12V_AGND_ V_GND_1 +3.3V_1 +5V_GND_1 +5V_1-12V_AGND_1-12V_1 +12V_AGND_1 +3.3V_GND_1 +3.3V_1 +5V_GND_1 +5V_1-12V_AGND_1-12V_1 +12V_AGND_1 ON/OFF SWITCHES CURRENT MONITOR. +3.3V_GND_1 +3.3V_1 +5V_GND_1 +5V_1-12V_AGND_1-12V_1 +12V_AGND_1 +12V_1 to XG-A More than 50 different DCDC Converters for Systems and Payloads, examples: Planetary Fourier Spectrometer for MEX and VEX 25W Power Supply Unit (fully redundant, 8 output rails, 3 separate returns, selfchecking of output voltages). Launched 2003 and 2005, still working in space. Plasma Wave Complex for DEMETER 20W Power Supply Unit for whole payload (10 output rails, complex system used for individual control and separation of the instruments, GAJA DCDC used). Launched in 2004, satellite switched off at the end of SIR2 IR Spectrometer in Chandrayaan Mission: 10W Power Supply Unit (7 rails, 3 separate returns, 1.5A/6W programmable current source, autonomous HK block). In operation 22 Oct Dec Miniature X and Gamma Ray Sensor (MXGS) in ASIM ISS Mission: 120W Power Supply Unit including high current supply rails for FPGA s, high stable supply rails for ASIC s/fea electronics and HV (100V 1kV) supply rails for detectors. Fully programmable by autonomous FPGA. Actually in Phase C/D. MEXIC Power Distribution Unit for TARANIS Mission: 60W Power Supply Unit dedicated for the whole TARANIS Payload. Actually in Phase C/D /
22 CBK PENETRATORS Credit ESA ESA Rosetta Spacecraft
23 CBK penetrators MUPUS KINETIC PENETRAROR TRAIL BLAZER Mole Penetrator CHOMIK
24 CBK hammer penetrators with EMDD OLD HEEP MUPUS CHOMIK NEW High Energy and Efficiency Penetrator E-MOLE
25 Phobos Sample Return Mission Our main task: to insert container into hard ground and collect a sample Container CHOMIK EQM in the Lab CHOMIK on the Russian manipulator
26 Features: Spacedrill drilling device Max. depth = 2m Storage of samples from entire length of the hole Sample size 1.5cm (diameter) x 6-7cm (height) Applications: Geological measurements (space) Tubular boom ø37 is needed
27 HEEP capabilities HEEP Tests in porous materials HEEP can easily break and penetrate porous materials. Tests with solid materials Solid rocks (e.g. granite) can be broken at their edge, generating pieces of few to 20 mm in size. Breaking Ø30x57mm block of YTONG Breaking pavement brick (compressive strength MPa) Breaking granite (compressive strength MPa)
28 TARGET SATELLITE WMS LEMUR ROBOTYKA ORBITALNA
29 thank you for your attention
30 BRITE-PL - the first Polish scientific satellite UTIAS/SFL Two satellites, designed and partially manufactured in SFL/UTIAS in Toronto, have been integrated and tested in SRC. Launches : November 2013 and May
31 Present status Three instruments plus one satellite are recently working in space: INTEGRAL, MEX, ROSETTA, BRITE-PL Lem Two instruments and one satellite are almost ready for launch: MERTIS/BepiColombo, OBSTANOVKA/ISS, BRITE-PL Heweliusz A few instruments are under development, in phase B or early C/D: RFA/RELEC, TARANIS, MXGS/ASIM, STIX/SolarOrbiter, HFA/RESONANCE, LAERT /JONOSFERA, RPW/JUICE, SWE/JUICE, CASSIS/ExoMars, CCB/PROBA
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