|
Delta-v budget (or velocity change budget) is a term used in astrodynamics and aerospace industry for velocity change (or delta-v) requirements for the various propulsive tasks and orbital maneuvers over phases of the space mission.
Sample delta-v budget will enumerate various classes of manoeuvres, delta-v per manoeuvre, number of manoeuvres required over the time of the mission.
In the absence of an atmosphere and landings where the ground is hit with some speed, the delta-v is the same for changes in orbit the other way around: gaining and losing speed cost an equal effort.
Launch/landing budget
- Launch to LEO — this not only requires an increase of velocity from 0 to 7.8 km/s, but also typically 1.5–2 km/s for atmospheric drag and gravity drag
- Re-entry from LEO
Stationkeeping budget
| Maneuver |
| Altitude |
| Average delta-v per year |
| Maximum m/s per year
|
| |
| [km] |
| [m/s] |
| [m/s] |
|
| station-keeping |
| |
| 50–55 |
|
|
| Drag compensation |
| 400–500 |
| <25 |
| <100 |
|
| Drag compensation |
| 500–600 |
| <5 |
| <25 |
|
| Drag compensation |
| >600 |
| |
| <7.5 |
|
| Attitude control (3-axis) |
| |
| 2–6 |
|
|
| Spin-up or despin |
| |
| 5–10 |
|
|
| Stage booster separation |
| |
| 5–10 |
|
|
| Momentum wheel unloading |
| |
| 2–6 |
|
|
| |
| |
|
|
|
Interplanetary budget
See also
External link
|