ExoMS

ExoMS - Propulsion

Our ExoMS – Propulsion offer allows you to understand what value propulsion can bring you ; what impact it has on your mission and on your system ; and how different technologies compare.

Mission profile

Single-plane or multi-plane phasing
Altitude transfer
Station keeping
Inclination correction
Deorbitation
Advanced concept

System specifications

Satellite weight
Satellite size, drag coefficient
Propulsion technology used (comparison possible)
Other

High-level requirements

Mission duration
Duty cycle
Satellite lifespan
Minimum thrust required
DeltaV / Total impulse required
Ergol mass required
Propulsion system volume
Comparison between different propulsion technologies

Detailed mission planning

Thrust & AOCS sequence
Detailed characteristics for each mission phase:
- DeltaV / Total Impulse
- Fuel consumption
- Battery energy consumption
- Distance to target
- RAAN to target
- Eccentricity to target
Trajectory optimisation
Orbital trajectory visualisation

ExoMS - Constellation

With our ExoMS – Constellation offer, you can analyse the performance of your constellations – whether they use propulsion or not.

Revisit rate / Coverage analysis
Evolution of performances with number of satellites, planes, altitude, launch strategy, ground station networks, propulsion,…
Constellation pre-design
First sizing & cost estimation for future telecom or earth observation projects