Table 2.
ΔV and propellant budget for the ADONIS mission.
| Spacecraft | ΔV (m/s) |
Propellant mass (kg) |
Margin (%) | ||
|---|---|---|---|---|---|
| A | B | A | B | ||
| Injection | 280 | 185 | 58 | 32 | 25 |
| Transit corrections | 5 | 100 | 2 | 28 | 35 |
| Orbit corrections | 500 | 500 | 75 | 75 | 40 |
| Avoidances | 100 | 100 | 15 | 15 | 10 |
| Total | 885 | 885 | 150 | 150 | 10 |
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