Astrodynamics

GPTKB entity

Statements (57)
Predicate Object
gptkbp:instanceOf gptkb:academic
gptkbp:alsoKnownAs celestial mechanics
gptkbp:appliesTo gptkb:Newton's_laws_of_motion
gptkb:law_of_universal_gravitation
gptkbp:hasConcept gptkb:restricted_three-body_problem
gptkb:Hill_sphere
gptkb:Hohmann_transfer
gptkb:Jacobi_constant
gptkb:Lambert's_problem
gptkb:gravity_assist
gptkb:Tsiolkovsky_rocket_equation
gptkb:orbital_maneuver
gptkb:sphere_of_influence
eccentricity
resonance
semi-major axis
orbital decay
escape velocity
argument of periapsis
delta-v
mean anomaly
orbital elements
orbital inclination
orbital period
orbital perturbations
patched conics
right ascension of ascending node
station-keeping
synodic period
transfer orbits
true anomaly
gptkbp:importantFor space debris tracking
satellite launches
space mission analysis
planetary flybys
orbital transfers
re-entry calculations
rendezvous and docking
space navigation
gptkbp:relatedTo gptkb:astronomy
aerospace engineering
physics
orbital mechanics
gptkbp:studies motion of artificial bodies in space
gptkbp:usedIn interplanetary mission planning
satellite orbit determination
spacecraft trajectory design
gptkbp:uses gptkb:n-body_problem
gptkb:perturbation_theory
gptkb:Lagrange_points
gptkb:Kepler's_laws
numerical integration
patched conic approximation
two-body problem
gptkbp:bfsParent gptkb:Lagrange_points
gptkbp:bfsLayer 6
https://www.w3.org/2000/01/rdf-schema#label Astrodynamics