| # |
Burn time |
DV |
Dt |
a |
| M0D | 2019-02-28 17:00:00.000 | 78.5 | 10.311 | 7.61 |
| M1D | 2019-03-02 17:00:00.000 | 36.9 | 4.958 | 7.43 |
| M2D | 2019-03-05 16:45:29.000 | 53.8 | 7.203 | 7.47 |
| M2D | 2019-03-05 17:14:31.000 | 53.9 | 7.230 | 7.45 |
| M3D | 2019-03-09 16:45:29.000 | 27.6 | 3.749 | 7.35 |
| M3D | 2019-03-09 17:14:31.000 | 27.7 | 3.751 | 7.38 |
| M4D | 2019-03-12 16:45:29.000 | 39.2 | 5.272 | 7.44 |
| M4D | 2019-03-12 17:14:31.000 | 39.1 | 5.288 | 7.39 |
| M5D | 2019-03-16 16:45:29.000 | 26.0 | 3.538 | 7.34 |
| M5D | 2019-03-16 17:14:31.000 | 26.2 | 3.547 | 7.40 |
| M6D | 2019-03-19 16:45:29.000 | 31.7 | 4.325 | 7.33 |
| M6D | 2019-03-19 17:14:31.000 | 31.8 | 4.348 | 7.32 |
| M7D | 2019-03-23 16:45:29.000 | 21.8 | 3.027 | 7.19 |
| M7D | 2019-03-23 17:14:31.000 | 21.8 | 3.038 | 7.17 |
| M8D | 2019-03-26 16:45:29.000 | 32.4 | 4.420 | 7.34 |
| M8D | 2019-03-26 17:14:31.000 | 32.5 | 4.425 | 7.35 |
| M9D | 2019-03-30 16:45:29.000 | 29.9 | 4.072 | 7.34 |
| M9D | 2019-03-30 17:14:31.000 | 29.9 | 4.090 | 7.32 |
| M10D | 2019-04-02 17:00:00.000 | 58.9 | 7.770 | 7.59 |
| M11D | 2019-04-06 16:45:29.000 | 47.7 | 6.373 | 7.48 |
| M11D | 2019-04-06 17:14:31.000 | 47.9 | 6.395 | 7.50 |
| M12D | 2019-04-09 17:00:00.000 | 59.9 | 7.877 | 7.60 |
The table shows the spacecraft maneuvers executed during this phase.
Most of the maneuvers were performed in two steps: one burn varies the trajectory and the other varies the speed (the magnitude of the velocity vector).
The graph shows the trajectory of the spacecraft in the Bennu-centric mean ecliptic and equinox of J2000 reference frame.
Poster (1.4 MiB pdf file) with detailed explanations:
Detailed Survey: Baseball Diamond
The popup label shows the date, the radius vector (km) and the spacecraft speed (mm/s).