near-rectilinear halo orbit (NRHO) around the Moon
GPTKB entity
Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:Moon
Lagrange point |
| gptkbp:advantage |
continuous line of sight to Earth
low fuel requirements for stationkeeping |
| gptkbp:closest_approach_to_Moon |
about 3,000 km
|
| gptkbp:farthest_distance_from_Moon |
about 70,000 km
|
| gptkbp:first_insertion_date |
November 2022 (CAPSTONE)
|
| gptkbp:first_spacecraft_to_use |
gptkb:CAPSTONE
|
| https://www.w3.org/2000/01/rdf-schema#label |
near-rectilinear halo orbit (NRHO) around the Moon
|
| gptkbp:orbit_shape |
highly elliptical
|
| gptkbp:period |
about 7 days
|
| gptkbp:plannedBy |
gptkb:Lunar_Gateway
|
| gptkbp:primary_body |
gptkb:Moon
|
| gptkbp:relatedTo |
gptkb:Lagrange_points
cislunar space |
| gptkbp:secondary_body |
gptkb:Earth
|
| gptkbp:stable |
highly stable
|
| gptkbp:type |
three-body orbit
|
| gptkbp:used_in |
gptkb:Lunar_Gateway
gptkb:NASA_Artemis_program |
| gptkbp:bfsParent |
gptkb:Power_and_Propulsion_Element_(PPE)
|
| gptkbp:bfsLayer |
6
|