Item Requirements
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Article Name: Purchase of an Electrical Simulator for ground test of 6-DOF
propulsion system for 6U nanosatel ite
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Type and Quantity
Item No.
Item
Q'ty
1
Electrical Simulator of 6-DOF propulsion system for 6U
nanosatel ite
Includes :
- Flight representative interface and control electronics board
- Components to simulate 6 thrusters and relevant parts of the storage and feed
system.
- Software package to control the 6-DOF propulsion system.
- Support
1 set
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Latest Delivery Date: February 21st, 2020
The contractor for the Electrical Simulator shal be capable of providing Flight Models of the
6-DOF propulsion system under a separate contract to be placed next year.
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Requirements
The fol owing requirements shal be applicable for the
6-DOF propulsion system and the
Electrical Simulator shall be aligned with these requirements where applicable:
The propulsion system shal be capable of providing 6-DOF motion of a 6U
nanosatel ite (this means translation along and rotation around al 3axis)
Size: Less than 2U (20x10x10cm) of total size
Mass: Less than 2kg
Mechanical Interface: The propulsion system must be suitable for standard 6U
cubesat shape (Redesign of the structure should be avoided)
Electrical interface:
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Communication shal be possible over these data buses: CAN, I2C, UART
Performance:
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Max thrust: 20mN for each axis
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Total Delta-V: around 16m/s (assuming a 10kg nanosatel ite)
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Capability to measure delivered impulse by each thruster in near real time
Quality & reliability:
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The propulsion system shal have flight heritage or equivalent qualification tests
performed
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Capability of meeting radiation requirements equivalent to 5 years in LEO (20
krad)
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Propulsion system design shal be compliant to the tailored ECSS standards for
IOD cubesat projects
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Al electrical components shal be de-rated according to ECSS standards
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The propulsion system shal have redundant sensors for al critical components
The Electrical Simulator shal mimic the FM module in a representative way, including
communication, thruster performance, thruster diagnostics, timing and sequencing of
commands, monitoring of propel ant tanks and feed system. More specifical y, the Electrical
Simulator shal have a ful y flight representative interface and control electronics board,
including identical connectors, so that the Electrical Simulator can replace the FM module in
a satel ite simulator or a flat-sat system.
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Payment terms
Payment for the contract shall be made as fol ows:
Ratio
Payment terms
50% ± 5%
After signing the contract
50% ± 5%
Deliver of al parts
