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Report Style: Maneuver History
Reports thrust maneuver metrics, as a function of time, during each Astrogator maneuver segment.Data Provider:Astrogator Maneuver Ephemeris Block History
Group:Maneuver
Type: Time-varying data. May supply data with duplicate times. Intended to be used only with elements from this same data provider.
Availability: Reports
Column Listing
| Column | Column Name | Element | Type | Dimension | Description |
|---|---|---|---|---|---|
| 1 | Time | Time | Real Number or Text | Date | Time. |
| 2 | DeltaV | DeltaV | Real Number | Speed Change | Delta-V magnitude integrated along the trajectory path. |
| 3 | FuelMass | FuelMass | Real Number | Mass | Fuel mass remaining. |
| 4 | Fuel_Density | Fuel_Density | Real Number | SmallDensity | Density of the fuel. |
| 5 | Specific_Impulse | Specific_Impulse | Real Number | SpecificImpulse | The specific impulse during the maneuver, accounting for all engines, computed using the rocket equation. |
| 6 | Tank_Pressure | Tank_Pressure | Real Number | Pressure | Fuel tank pressure. |
| 7 | Tank_Temperature | Tank_Temperature | Real Number | Temperature | Fuel tank temperature. |
| 8 | Total_Mass | Total_Mass | Real Number | Mass | Total mass (fuel plus dry mass). |
| 9 | Total_Mass_Flow_Rate | Total_Mass_Flow_Rate | Real Number | Mass Per Time | The total mass flow rate, accounting for all engines, during a maneuver. |