near-rectilinear halo orbit (NRHO)
GPTKB entity
Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:Moon
gptkb:Titan Lagrange point |
| gptkbp:centralTo |
gptkb:Earth-Moon_system
|
| gptkbp:characterizedBy |
highly elliptical shape
stability with low fuel requirements |
| gptkbp:closest_approach_to_Moon |
about 3,000 km
|
| gptkbp:enables |
access to lunar south pole
continuous line-of-sight to Earth |
| gptkbp:farthest_distance_from_Moon |
about 70,000 km
|
| gptkbp:first_spacecraft_to_use |
gptkb:CAPSTONE
|
| https://www.w3.org/2000/01/rdf-schema#label |
near-rectilinear halo orbit (NRHO)
|
| gptkbp:period |
about 6.5 days
|
| gptkbp:proposedBy |
future lunar missions
|
| gptkbp:relatedTo |
gptkb:Lagrange_points
cislunar space |
| gptkbp:studiedBy |
gptkb:NASA
gptkb:ESA |
| gptkbp:type |
three-body orbit
|
| gptkbp:used_in |
gptkb:Lunar_Gateway
gptkb:NASA_Artemis_program |
| gptkbp:bfsParent |
gptkb:Lunar_Gateway
|
| gptkbp:bfsLayer |
5
|