Classifier Instance:

Anchor text: LEO
Target Entity: Low_Earth_orbit
Preceding Context: Also, for a given objective such as moving from one orbit to another, the required \Delta v may depend greatly on the rate at which the engine can produce \Delta v and maneuvers may even be impossible if that rate is too low. For example, a launch to
Succeeding Context: normally requires a \Delta v of ca. 9.5 km/s (mostly for the speed to be acquired), but if the engine could produce \Delta v at a rate of only slightly more than g, it would be a slow launch requiring altogether a very large \Delta v (think of hovering without making any progress in speed or altitude, it would cost a \Delta v of 9.8 m/s each second). If the possible rate is only g or less, the maneuver can not be carried out at all with this engine.
Paragraph Title: null
Source Page: Spacecraft propulsion

Ground Truth Types:

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|  |  |---wordnet_location_100027167
|  |  |  |---wordnet_line_108593262
|  |  |  |  |---wordnet_path_108616311

Predicted Types:

wordnet_artifact_100021939-0.0335320004167013 0
wordnet_event_100029378-1.404916493638865 0
wordnet_organization_108008335-1.481517973314935 0
wordnet_person_100007846-0.027818919513336045 0
yagoGeoEntity-0.818863713904039 0
|  |---wordnet_artifact_100021939
|  |---wordnet_event_100029378
|  |---wordnet_organization_108008335
|  |---wordnet_person_100007846
|  |---yagoGeoEntity