Hohmann transfer orbit

GPTKB entity

Statements (61)
Predicate Object
gptkbp:instance_of gptkb:battle
gptkbp:allows the positions of celestial bodies
gptkbp:analyzes a two-burn trajectory
gptkbp:applies_to geostationary satellites
all celestial bodies
https://www.w3.org/2000/01/rdf-schema#label Hohmann transfer orbit
gptkbp:involves a periapsis and an apoapsis
gptkbp:is_a_way_to maximize mission success
specific orbital parameters
gptkbp:is_affected_by gravitational perturbations
gptkbp:is_characterized_by an elliptical orbit
gptkbp:is_effective_against bi-impulsive transfer
low-energy transfers
gptkbp:is_essential_for efficient space travel
gptkbp:is_evaluated_by gptkb:Kepler's_laws
gptkbp:is_fundamental_to astrodynamics
spacecraft navigation
gptkbp:is_often_compared_to other transfer methods
gptkbp:is_often_used_in gptkb:spacecraft
gravity assists
low Earth orbit missions
inter-orbital transfers
gptkbp:is_optimized_for specific mission profiles
cost efficiency.
propellant usage
transfers between circular orbits
gptkbp:is_tasked_with deep space missions
mission planning software
gptkbp:is_used_for Newton's laws of motion
transferring between two orbits
reach planets
gptkbp:is_used_in satellite deployment
gptkbp:is_used_to transfer spacecraft
gptkbp:key gptkb:spacecraft
gptkbp:marketing_strategy fuel conservation
gptkbp:named_after gptkb:Walter_Hohmann
a German engineer
gptkbp:performed_by a vacuum
gptkbp:proposed_by gptkb:Walter_Hohmann
gptkbp:propulsion spacecraft propulsion systems
minimal energy expenditure
gptkbp:requires two engine burns
gptkbp:skills gptkb:orbital_mechanics
gptkbp:tactics commercial spaceflight
different spacecraft designs
gptkbp:technique satellite constellations
precise timing
scientific exploration
interplanetary travel
return missions
various space missions
orbital insertion
changing orbital planes
orbital simulation tools
gptkbp:type_of transfer orbit
elliptical transfer orbit
gptkbp:bfsParent gptkb:New_Horizons
gptkb:Vega_1
gptkb:Aldrin's_Mars_Cycler
gptkb:Bepi_Colombo
gptkbp:bfsLayer 4