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Delta-v (also known as "change in velocity"), symbolized as Δ v {\textstyle {\Delta v}} and pronounced /dɛltə viː/, as used in spacecraft flight dynamics, is a measure of the impulse per unit of spacecraft mass that is needed to perform a maneuver such as launching from or landing on a planet or moon, or an in-space orbital maneuver. It is a scalar that…
Measurement, Delta-v budgets & Overview
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mass spacecraft velocity thrust rocket change maneuvers propellant required displaystyle orbit used also orbital example time equation per fuel acceleration
| Subject | Predicate | Object | Confidence | Src |
|---|---|---|---|---|
| Delta-v | is a | same as for the non-reversed thrust.For rockets | 0.90 | text |
| Delta-v | is a | magnitude of the acceleration caused by the engines | 0.90 | text |
| launching from or landing on a planet or moon | instance of | is a measure of the impulse per unit of spacecraft mass that is needed to perform a maneuver | 0.80 | text |
| or an in-space orbital maneuver | instance of | is a measure of the impulse per unit of spacecraft mass that is needed to perform a maneuver | 0.80 | text |
| Delta-v | related to Around the Solar System | Lower-delta-v | 0.60 | section |
| Delta-v | related to Around the Solar System | Orbital | 0.60 | section |
| Delta-v | related to Around the Solar System | Interplanetary Transport Network | 0.60 | section |
| Delta-v | related to Delta-v budgets | When | 0.60 | section |
| Delta-v | related to Delta-v budgets | Propellant | 0.60 | section |
| Delta-v | related to Delta-v budgets | It | 0.60 | section |
| Delta-v | related to Delta-v budgets | For | 0.60 | section |
| Delta-v | related to Delta-v budgets | Earth's | 0.60 | section |
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