All Topics  
Characteristic energy

 

   Email Print
   Bookmark   Link






 

Characteristic energy



 
 
In astrodynamics
Astrodynamics

Orbital mechanics or astrodynamics is the application of celestial mechanics to the practical problems concerning the motion of rockets and other spacecraft....
 a characteristic energy is a measure of the energy required for an interplanetary mission that requires attaining an excess orbital velocity over an escape velocity
Escape velocity

In physics, escape velocity is the speed where the kinetic energy of an object is equal to the magnitude of its gravitational potential energy, as calculated by the equation,...
 required for additional orbital maneuver
Orbital maneuver

In spaceflight, an orbital maneuver is the use of spacecraft propulsion systems to change the orbit of a spacecraft. For spacecraft far from Earth -- for example those in orbits around the Sun -- an orbital maneuver is called a deep-space maneuver ....
s. The unit of the characteristic energy is km
Kilometre

The kilometre , symbol km is a Units of measurement of length in the metric system, equal to one thousand metres.Slang terms for kilometre include click and kay ....
2s
Second

The second , sometimes abbreviated sec., is the name of a units of measurement of time, and is the International System of Units SI base unit of time....
-2.

Characteristic energy can be computed as:

where

is the orbital velocity when the orbital distance tends to infinity.






Discussion
Ask a question about 'Characteristic energy'
Start a new discussion about 'Characteristic energy'
Answer questions from other users
Full Discussion Forum



Encyclopedia


In astrodynamics
Astrodynamics

Orbital mechanics or astrodynamics is the application of celestial mechanics to the practical problems concerning the motion of rockets and other spacecraft....
 a characteristic energy is a measure of the energy required for an interplanetary mission that requires attaining an excess orbital velocity over an escape velocity
Escape velocity

In physics, escape velocity is the speed where the kinetic energy of an object is equal to the magnitude of its gravitational potential energy, as calculated by the equation,...
 required for additional orbital maneuver
Orbital maneuver

In spaceflight, an orbital maneuver is the use of spacecraft propulsion systems to change the orbit of a spacecraft. For spacecraft far from Earth -- for example those in orbits around the Sun -- an orbital maneuver is called a deep-space maneuver ....
s. The unit of the characteristic energy is km
Kilometre

The kilometre , symbol km is a Units of measurement of length in the metric system, equal to one thousand metres.Slang terms for kilometre include click and kay ....
2s
Second

The second , sometimes abbreviated sec., is the name of a units of measurement of time, and is the International System of Units SI base unit of time....
-2.

Characteristic energy can be computed as:

where

is the orbital velocity when the orbital distance tends to infinity. Note that, since the kinetic energy is one half m C3 is in fact equal to twice the magnitude of the specific energy
Specific orbital energy

In astrodynamics the specific orbital energy of an orbiting body traveling through space under standard assumptions in astrodynamics is the sum of its potential energy and kinetic energy per unit mass....
  of the escaping object.

Parabolic trajectory

For a spacecraft that is leaving the central body
Central body

In astrodynamics a central body is a body that is being orbited by an orbiting body . Under standard assumptions in astrodynamics:* it is more massive than the orbiting body by several orders of magnitude ,...
 (e.g. earth) on a parabolic trajectory
Parabolic trajectory

In astrodynamics or celestial mechanics a parabolic trajectory is a Kepler orbit with the eccentricity equal to 1. When moving away from the source it is called an escape orbit, otherwise a capture orbit....
:

Hyperbolic trajectory

For a spacecraft that is leaving the central body
Central body

In astrodynamics a central body is a body that is being orbited by an orbiting body . Under standard assumptions in astrodynamics:* it is more massive than the orbiting body by several orders of magnitude ,...
 on a hyperbolic trajectory
Hyperbolic trajectory

In astrodynamics or celestial mechanics a hyperbolic trajectory is a Kepler orbit with the eccentricity greater than 1. Under standard assumptions in astrodynamics a body traveling along this trajectory will orbital coast to infinity, arriving there with hyperbolic excess velocity relative to the central body....
:

where:

is standard gravitational parameter
Standard gravitational parameter

In astrodynamics, the standard gravitational parameter of a celestial body is the product of the gravitational constant and the mass :The units of the standard gravitational parameter are km3s-2...
,

is length of semi-major axis
Semi-major axis

In geometry, the semi-major axis is used to describe the dimensions of ellipses and hyperbolae....
 of orbit
ORBit

ORBit is a Common Object Request Broker Architecture 2.4 compliant Object Request Broker . It features mature C , C++ and Python bindings, and less developed bindings for Perl, Lisp , Pascal , Ruby , and Tcl....
's hyperbola
Hyperbola

In mathematics a hyperbola is a smooth function planar curve having two connected components or branches, each a mirror image of the other and resembling two infinite bow aimed at each other....
.

See also

  • Specific orbital energy
    Specific orbital energy

    In astrodynamics the specific orbital energy of an orbiting body traveling through space under standard assumptions in astrodynamics is the sum of its potential energy and kinetic energy per unit mass....
  • Orbit
    ORBit

    ORBit is a Common Object Request Broker Architecture 2.4 compliant Object Request Broker . It features mature C , C++ and Python bindings, and less developed bindings for Perl, Lisp , Pascal , Ruby , and Tcl....
  • Parabolic trajectory
    Parabolic trajectory

    In astrodynamics or celestial mechanics a parabolic trajectory is a Kepler orbit with the eccentricity equal to 1. When moving away from the source it is called an escape orbit, otherwise a capture orbit....
  • Hyperbolic trajectory
    Hyperbolic trajectory

    In astrodynamics or celestial mechanics a hyperbolic trajectory is a Kepler orbit with the eccentricity greater than 1. Under standard assumptions in astrodynamics a body traveling along this trajectory will orbital coast to infinity, arriving there with hyperbolic excess velocity relative to the central body....