Statements (19)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:mathematical_concept
|
| gptkbp:appliesTo |
gptkb:Keplerian_orbits
|
| gptkbp:describes |
relationship between time of flight and orbital parameters
|
| gptkbp:field |
celestial mechanics
|
| gptkbp:namedAfter |
gptkb:Johann_Heinrich_Lambert
|
| gptkbp:publishedIn |
18th century
|
| gptkbp:relatedTo |
semi-major axis
chord length elliptical, parabolic, and hyperbolic orbits sum of distances to foci transfer time |
| gptkbp:usedFor |
orbit determination
interplanetary trajectory planning |
| gptkbp:usedIn |
gptkb:astrodynamics
space mission design |
| gptkbp:bfsParent |
gptkb:Lambert
gptkb:Johann_Heinrich_Lambert |
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Lambert's theorem
|