Statements (18)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
orbital maneuver
|
| gptkbp:assumes |
coplanar circular orbits
instantaneous velocity changes |
| gptkbp:firstDescribed |
1925
|
| https://www.w3.org/2000/01/rdf-schema#label |
Hohmann transfer
|
| gptkbp:involves |
two engine impulses
|
| gptkbp:namedAfter |
gptkb:Walter_Hohmann
|
| gptkbp:reduces |
delta-v for coplanar orbits
|
| gptkbp:relatedTo |
gptkb:satellite
orbital mechanics bi-elliptic transfer |
| gptkbp:usedFor |
interplanetary travel
satellite orbit change spacecraft trajectory change |
| gptkbp:bfsParent |
gptkb:Astrodynamics
gptkb:Trans-lunar_injection gptkb:Geostationary_Transfer_Orbit |
| gptkbp:bfsLayer |
6
|