// ORBITAL LOGISTICS AND PROPULSION TERM
Mass Fraction
Mass fraction is a way to describe how much of a specific ingredient is in a mixture, expressed as a percentage or decimal of the total mass. For example, if a rocket's fuel is 80% of its total mass, its fuel mass fraction is 0.8.
TECHNICAL DEFINITION
Mass fraction (mf) quantifies the proportion of a specific component's mass relative to the total mass of a mixture or system, commonly used in propulsion to assess propellant loading or structural efficiency.
BACKGROUND
A space settlement is a settlement in outer space, sustaining more extensively habitation facilities in space than a general space station or spacecraft. Possibly including closed ecological systems, its particular purpose is permanent habitation.
READ MORE ON WIKIPEDIASYNONYMS & ALIASES
- mass percentage
- mass ratio (component)
- weight fraction
USAGE NOTE
In rocket design, a high propellant mass fraction is desirable for maximizing performance.
DEVELOPERS
Organizations developing technology related to Mass Fraction.
Develops high-performance engines like Raptor and advanced materials like custom stainless steel alloys for its Starship vehicle, all aimed at minimizing structural weight to maximize the propellant and payload capacity.
Pioneered the use of carbon composite materials for the entire primary structure and propellant tanks of its Electron launch vehicle, a direct strategy to reduce dry mass and improve the overall mass fraction.
Utilizes large-scale 3D printing to manufacture its rocket structures. This approach allows for the creation of lightweight, integrated components with optimized geometries, reducing part count and structural mass.
Constructs its Alpha rocket using all-carbon-composite structures, including propellant tanks and the main airframe, to achieve a very low structural mass and a high performance-to-weight ratio.
Researches and develops advanced materials and manufacturing techniques to improve mass fraction for space missions. Examples include lightweight aluminum-lithium alloys for the Space Launch System (SLS) tanks and work on composite cryotanks.
Engineers highly efficient upper stages like the Centaur, which has a long heritage of using pressure-stabilized, thin-walled stainless steel tanks and common bulkheads to achieve an industry-leading mass fraction.
Is developing a fully reusable upper stage with a novel design that integrates propulsion and thermal protection systems. This architecture aims to drastically reduce the dry mass typically required for reusable heat shields and hardware.