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- Propellant_mass_fraction abstract "In aerospace engineering, the propellant mass fraction is the portion of a vehicle's mass which does not reach the destination, usually used as a measure of the vehicle's performance. In other words, the propellant mass fraction is the ratio between the propellant mass and the initial mass of the vehicle. In a spacecraft, the destination is usually an orbit, while for aircraft it is their landing location. A higher mass fraction represents less weight in a design. Another related measure is the payload fraction, which is the fraction of initial weight that is payload.".
- Propellant_mass_fraction wikiPageID "309304".
- Propellant_mass_fraction wikiPageRevisionID "574679645".
- Propellant_mass_fraction hasPhotoCollection Propellant_mass_fraction.
- Propellant_mass_fraction subject Category:Astrodynamics.
- Propellant_mass_fraction subject Category:Mass.
- Propellant_mass_fraction subject Category:Rocket_propulsion.
- Propellant_mass_fraction subject Category:Single-stage-to-orbit.
- Propellant_mass_fraction comment "In aerospace engineering, the propellant mass fraction is the portion of a vehicle's mass which does not reach the destination, usually used as a measure of the vehicle's performance. In other words, the propellant mass fraction is the ratio between the propellant mass and the initial mass of the vehicle. In a spacecraft, the destination is usually an orbit, while for aircraft it is their landing location. A higher mass fraction represents less weight in a design.".
- Propellant_mass_fraction label "Propellant mass fraction".
- Propellant_mass_fraction sameAs m.01sz9r.
- Propellant_mass_fraction sameAs Q7250140.
- Propellant_mass_fraction sameAs Q7250140.
- Propellant_mass_fraction wasDerivedFrom Propellant_mass_fraction?oldid=574679645.
- Propellant_mass_fraction isPrimaryTopicOf Propellant_mass_fraction.