Statements (18)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
orbital maneuver
|
| gptkbp:appliesTo |
elliptical orbits
coplanar orbits |
| gptkbp:category |
gptkb:astrodynamics
|
| gptkbp:describedBy |
Die Erreichbarkeit der Himmelskörper
|
| gptkbp:firstDescribed |
1925
|
| https://www.w3.org/2000/01/rdf-schema#label |
Hohmann transfer orbit
|
| gptkbp:namedAfter |
gptkb:Walter_Hohmann
|
| gptkbp:reduces |
delta-v for transfer
|
| gptkbp:relatedTo |
gptkb:satellite
orbital mechanics bi-elliptic transfer |
| gptkbp:requires |
two engine impulses
|
| gptkbp:usedFor |
fuel-efficient orbital transfer
spacecraft transfer between two orbits |
| gptkbp:usedIn |
space missions
|
| gptkbp:bfsParent |
gptkb:Walter_Hohmann
|
| gptkbp:bfsLayer |
7
|