Properties (48)
Predicate | Object |
---|---|
gptkbp:instanceOf |
scientific laws
|
gptkbp:appliesTo |
natural satellites
artificial satellites satellites of planets |
gptkbp:description |
the motion of celestial bodies
|
gptkbp:has_a_focus_on |
academic research
|
https://www.w3.org/2000/01/rdf-schema#label |
Cassini's Laws
|
gptkbp:includes |
three laws
|
gptkbp:influenced |
gravitational interactions
|
gptkbp:influences |
orbital mechanics
|
gptkbp:is_a_platform_for |
celestial mechanics
space mission analysis orbital insertion techniques spacecraft trajectory design |
gptkbp:is_a_route_for |
satellite deployment strategies
|
gptkbp:is_a_subject_of |
research papers
scientific conferences astrodynamics academic discussions |
gptkbp:is_essential_for |
space exploration
mission success satellite navigation systems launch window calculations understanding satellite dynamics |
gptkbp:is_involved_in |
planetary ring dynamics
|
gptkbp:is_part_of |
classical mechanics
|
gptkbp:is_referenced_in |
textbooks on astronomy
orbital design |
gptkbp:is_studied_in |
graduate astronomy courses
|
gptkbp:is_used_in |
astrophysics
simulation software space mission planning satellite behavior |
gptkbp:isConnectedTo |
tidal forces
|
gptkbp:isUsedFor |
gptkb:Newton's_laws_of_motion
|
gptkbp:legal_principle |
spacecraft rendezvous missions
the line joining a satellite and the planet sweeps out equal areas in equal times the orbit of a satellite is an ellipse the square of the orbital period of a satellite is proportional to the cube of the semi-major axis of its orbit |
gptkbp:previousName |
gptkb:Giovanni_Domenico_Cassini
|
gptkbp:related_to |
gptkb:Kepler's_laws_of_planetary_motion
planetary science orbital stability orbital perturbations orbital transfer maneuvers |
gptkbp:suitableFor |
exoplanetary systems
engineering of spacecraft |
gptkbp:traditions |
spacecraft operations
|