PROGRAM 01 / 03
ESA · Earth Observation · 2018
A high-resolution imaging satellite tracking climate and land-use change. Led the primary structural bus and payload integration—from raw composite panels to a flight-qualified spacecraft.
SCROLL TO ASSEMBLE
Built to a tenth of a millimetre.
PRIMARY STRUCTURE
CFRP sandwich panels with aluminium honeycomb core, titanium fittings at all major load interfaces.
POINTING ACCURACY
Better than 0.03° three-axis stabilisation, validated across the full thermal-vacuum envelope.
QUALIFICATION
Sine & random vibration, acoustic, and 14-day thermal-vacuum cycling to ESA ECSS standards.
PROGRAM PARTNERS