| Project Name |
Delivery |
Launch date |
Customer |
Description |
|
DIMAC FM
|
2007 |
09/2007 |
ESA |
Proto-flight development for Foton M-3 flight providing:
- vibration sensor and autonomous data acquisition system
(enhanced TAS3, internal magnetometer, 10GByte data storage)
- experimental quasi-steady acceleration sensor
- magnetometer sensors at 3 remote locations
Mission support, data analysis and reporting (see results summary).
|
|
TAS3
|
2005
2007 |
05/2005 |
ESA |
Proto-flight development of a triaxial accelerometer system for the Foton-M2 flight. Features
autonomous data acquisition and 8GByte data storage capacity.
Mission data analysis and reporting (see results summary).
Expansion with DIMAC electronics modules for the Foton M-3 flight. |
|
DIMAC study
|
2005
2005 |
N/A |
ESA |
Study and prototype development of a (quasi)-steady-state microgravity
acceleration measurement device. Participation to parabolic flight campaign with DIMAC prototype.
|
|
MMA
|
2003 |
02/2008 |
Verhaert |
Proto-flight development of a microgravity accelerometer package
for FSL core facility (Columbus module - ISS). |
TAS2 / TAS2-bis
|
2002 2004 |
10/2002 05/2005 |
ESA |
Proto-flight development of a replacement of the FluidPac tri-axial accelerometer
subsystem for the FluidPac re-flight (Foton M-1 flight). Rebuild hardware after launch
failure (for Foton M-2 flight). |
ALSM / ALSM2
|
2000 2002 |
N/A |
Verhaert |
GSE development (cooling air loop simulator module) for the FSL facility.
First unit for FSL engineering model, second (upgraded) unit for FSL flight model. |
|
FluidPac
|
2001 |
10/2002 |
Verhaert |
Consultancy in the frame of the FluidPac facility re-flight
(Foton M-1 flight, launch failed). |