Template:Astrodynamics

Astrodynamics
Part of a series on

Orbital mechanics
Orbital elements Apsis Argument of periapsis Eccentricity Inclination Mean anomaly Orbital nodes Semi-major axis True anomaly
Types of two-body orbits by eccentricity Circular orbit Elliptic orbit Transfer orbit (Hohmann transfer orbit Bi-elliptic transfer orbit) Parabolic orbit Hyperbolic orbit Radial orbit Decaying orbit
Equations Dynamical friction Escape velocity Kepler's equation Kepler's laws of planetary motion Orbital period Orbital velocity Surface gravity Specific orbital energy Vis-viva equation
Celestial mechanics
Gravitational influences Barycenter Hill sphere Perturbations Sphere of influence
N-body orbits Lagrangian points (Halo orbits) Lissajous orbits Lyapunov orbits
Engineering and efficiency
Preflight engineering Mass ratio Payload fraction Propellant mass fraction Tsiolkovsky rocket equation
Efficiency measures Gravity assist Oberth effect
Propulsive maneuvers Orbital maneuver Orbit insertion
v t e

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Astrodynamics
Part of a series on

Orbital mechanics
Orbital elements Apsis Argument of periapsis Eccentricity Inclination Mean anomaly Orbital nodes Semi-major axis True anomaly
Types of two-body orbits by eccentricity Circular orbit Elliptic orbit Transfer orbit (Hohmann transfer orbit Bi-elliptic transfer orbit) Parabolic orbit Hyperbolic orbit Radial orbit Decaying orbit
Equations Dynamical friction Escape velocity Kepler's equation Kepler's laws of planetary motion Orbital period Orbital velocity Surface gravity Specific orbital energy Vis-viva equation
Celestial mechanics
Gravitational influences Barycenter Hill sphere Perturbations Sphere of influence
N-body orbits Lagrangian points (Halo orbits) Lissajous orbits Lyapunov orbits
Engineering and efficiency
Preflight engineering Mass ratio Payload fraction Propellant mass fraction Tsiolkovsky rocket equation
Efficiency measures Gravity assist Oberth effect
Propulsive maneuvers Orbital maneuver Orbit insertion
v t e

Usage

As per the Manual of Style, place this template at the top of astrodynamics-related pages, just before the lead.

This template includes collapsible lists.

• To set it to display all lists when it appears (i.e. all lists expanded), use:
{{Astrodynamics |expanded=all}} or, if enabled, {{Astrodynamics |all}} (i.e. omitting "expanded=").

• To set it to display one particular list while keeping the remainder collapsed (i.e. hidden apart from their headings), use:
{{Astrodynamics |expanded=listname}} or, if enabled, {{Astrodynamics |listname}}
…where listname is one of the following (do not include any quotemarks):
Orbital elements, Types of two-body orbits by eccentricity, Equations, Gravitational influences, N-body orbits, Preflight engineering, Efficiency measures
For example, {{Astrodynamics |expanded=Gravitational influences}} or, if enabled, {{Astrodynamics |Gravitational influences}}

The above documentation is transcluded from Template:Astrodynamics/doc.
Editors can experiment in this template's sandbox and testcases pages.
Add categories to the /doc subpage. Subpages of this template.