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Transfer orbit used to reach geosynchronous or geostationary orbit
design, a geostationary transfer orbit (GTO) or geosynchronous transfer orbit is a highly elliptical type of geocentric orbit, usually with a perigee
Geostationary_transfer_orbit
Transfer manoeuvre between two orbits
astronautics, the Hohmann transfer orbit (/ˈhoʊmən/) is an orbital maneuver used to transfer a spacecraft between two orbits of different altitudes around
Hohmann_transfer_orbit
Elliptical orbit used to move a spacecraft from one circular orbit to another
In orbital mechanics, a transfer orbit is an intermediate elliptical orbit that is used to move a spacecraft in an orbital maneuver from one circular
Transfer_orbit
Orbit around the barycenter of the Sun
heliocentric orbit (also called circumsolar orbit) is an orbit around the Sun. The inner planets are mainly influenced by the Sun's gravity, and orbit points
Heliocentric_orbit
Propulsive maneuver used to arrive at the Moon
the lunar transfer arc, its trajectory approximates an elliptical orbit about the Earth with an apogee near to the radius of the Moon's orbit. The TLI
Trans-lunar_injection
Movement during spaceflight
Earth, an orbital maneuver is called a deep-space maneuver (DSM). When a spacecraft is not conducting a maneuver, especially in a transfer orbit, it is said
Orbital_maneuver
geosynchronous orbit. Parking orbit, a temporary orbit. Transfer orbit, an orbit used during an orbital maneuver from one orbit to another. Lunar transfer orbit (LTO)[clarification
List_of_orbits
Field of classical mechanics concerned with the motion of spacecraft
comets. Orbital mechanics focuses on spacecraft trajectories, including orbital maneuvers, orbital plane changes, and interplanetary transfers, and is
Orbital_mechanics
Spacecraft end-of-life orbit
the graveyard orbit is a few hundred kilometers beyond the operational orbit. The transfer to a graveyard orbit beyond geostationary orbit requires the
Graveyard_orbit
Orbit of an object around the Moon
spaceflight, a lunar orbit (also known as a selenocentric orbit) is an orbit by an object around Earth's Moon. In general these orbits are not circular.
Lunar_orbit
Type of orbital maneuver
aerospace engineering, the bi-elliptic transfer is an orbital maneuver that moves a spacecraft from one orbit to another and may, in certain situations
Bi-elliptic_transfer
Type of co-orbital motion of a small orbiting body relative to a larger orbiting body
horseshoe orbit of (419624) 2010 SO16 around the Earth-Sun system over 900 years In celestial mechanics, a horseshoe orbit is a type of co-orbital motion
Horseshoe_orbit
Quasi-periodic orbital trajectory
Weir, a Lissajous orbit is used as a transfer point for routine travel to and from the Moon. Libration point orbit Possibly a halo orbit. Sources disagree
Lissajous_orbit
Speed at which a body orbits around the barycenter of a system
the orbital speed of an astronomical body or object (e.g. planet, moon, artificial satellite, spacecraft, or star) is the speed at which it orbits around
Orbital_speed
Orbit keeping the satellite at a fixed longitude above the equator
A geosynchronous orbit (sometimes abbreviated GEO) is an Earth-centered orbit with an orbital period that matches Earth's rotation on its axis, 23 hours
Geosynchronous_orbit
Kepler orbit with an eccentricity of less than one
elongated orbit (e near 1). Examples of elliptic orbits or trajectories for satellites include Hohmann transfer orbits, Molniya orbits, and tundra orbits. Under
Elliptic_orbit
Spacecraft used to transfer cargo from one orbit to another
A space tug is a type of spacecraft used to transfer spaceborne cargo from one orbit to another orbit with different energy characteristics. The term
Space_tug
Orbit in the two body case with high eccentricity
call these orbits "elongated" than "highly elliptical". Highly eccentric orbits have two main uses - as transfer orbits and as good orbits for communication
Highly_elliptical_orbit
Jodi Sorensen (15 July 2020). "Spaceflight Inc. unveiled next-gen orbital transfer vehicle to fly aboard latest SpaceX rideshare mission". Spaceflight
List of Falcon 9 and Falcon Heavy launches (2020–2022)
List_of_Falcon_9_and_Falcon_Heavy_launches_(2020–2022)
Spaceflight operation
acceleration to reach orbital speed. Higher energy orbits like geostationary orbit are often reached via elliptical transfer orbits. One type of orbit insertion is
Orbit_insertion
Temporary orbit used during the launch of a spacecraft
Geostationary spacecraft require an orbit in the plane of the equator. Getting there requires a geostationary transfer orbit with an apogee directly above the
Parking_orbit
Orbit around Earth
A geocentric orbit, Earth-centered orbit, or Earth orbit involves any object orbiting Earth, such as the Moon or artificial satellites. In 1997, NASA estimated
Geocentric_orbit
Equilibrium points near two orbiting bodies
L. Gay See the Lagrange Points and Halo Orbits subsection under the section on Geosynchronous Transfer Orbit in NASA: Basics of Space Flight, Chapter
Lagrange_point
Orbit with a fixed distance from the barycenter
needed for the orbital speed of the circular orbit. It is also a matter of maneuvering into the orbit. See also Hohmann transfer orbit. In Schwarzschild
Circular_orbit
Fuel-efficient orbital maneuver
A low-energy transfer, or low-energy trajectory, is a route in space that allows spacecraft to change orbits using significantly less fuel than traditional
Low-energy_transfer
Type of geocentric orbit
A Sun-synchronous orbit (SSO), also called a heliosynchronous orbit, is a nearly polar orbit around a planet, in which the satellite passes over any given
Sun-synchronous_orbit
Periodic, three-dimensional orbit
Halo orbit A halo orbit is a periodic, non-planar orbit associated with one of the L1, L2 or L3 Lagrange points in the three-body problem of orbital mechanics
Halo_orbit
Process that leads to gradual decrease of the distance between two orbiting bodies
Orbital decay is a gradual decrease of the distance between two orbiting bodies at their closest approach (the periapsis) over many orbital periods. These
Orbital_decay
Estimate of total change in velocity of a space mission
although more fuel is needed to transfer a heavier communication satellite from low Earth orbit to geosynchronous orbit than for a lighter one, the delta-v
Delta-v_budget
Periodic, three-dimensional orbit
In orbital mechanics a near-rectilinear halo orbit (NRHO) is a halo orbit that passes close to the smaller of two bodies and has nearly stable behavior
Near-rectilinear_halo_orbit
Trajectory of Earth around the Sun
Earth orbits the Sun at an average distance of 149.60 million km (92.96 million mi), or 8.317 light-minutes, in a counterclockwise direction as viewed
Earth's_orbit
Movement around a celestial body that remains below its Karman line
orbit (TAO) is an orbit around a celestial body in which a portion of the orbit intersects with the defined atmosphere. Transatmospheric Earth orbits
Transatmospheric_orbit
Kind of planetary orbit
A supersynchronous orbit is either an orbit with a period greater than that of a synchronous orbit, or just an orbit whose major axis is larger than that
Supersynchronous_orbit
2013. "SpaceX Successfully Completes First Mission to Geostationary Transfer Orbit". SpaceX. 3 December 2013. Archived from the original on 29 December
List of Falcon 9 and Falcon Heavy launches (2010–2019)
List_of_Falcon_9_and_Falcon_Heavy_launches_(2010–2019)
Curved path of an object around a point
mechanics, an orbit is the curved trajectory of an object under the influence of an attracting force. Alternatively, it is known as an orbital revolution
Orbit
Single-stage solid-fueled booster rocket
The Transfer Orbit Stage (TOS) was an upper stage developed by Martin Marietta for Orbital Sciences Corporation during the late 1980s and early 1990s.
Transfer_Orbit_Stage
Type of spacecraft orbit
low-energy cislunar orbit transfers between a near-rectilinear halo orbit (NRHO) and a distant retrograde orbit (DRO) and orbit maintenance for a period
Distant_retrograde_orbit
Orbit around Earth between 160 and 2000 km
A low Earth orbit (LEO) is an orbit around Earth with a period of 128 minutes or less (making at least 11.25 orbits per day) and an eccentricity less
Low_Earth_orbit
Time an astronomical object takes to complete one orbit around another object
The orbital period (also revolution period) is the amount of time a given astronomical object takes to complete one orbit around another object. In astronomy
Orbital_period
Spaceflight maneuver
Orbital inclination change is an orbital maneuver aimed at changing the inclination of an orbiting body's orbit. This maneuver is also known as an orbital
Orbital_inclination_change
Measure of amount of effort to change trajectory
fuzzy orbits. C3 Escape orbit GEO Geosynchronous orbit GTO Geostationary transfer orbit L4/5 Earth–Moon L4L5 Lagrangian point LEO Low Earth orbit For example
Delta-v
Earth-centered orbit above low Earth orbit and below geostationary orbit
A medium Earth orbit (MEO) is an Earth-centered orbit with an altitude above a low Earth orbit (LEO) and below a high Earth orbit (HEO) – between 2,000
Medium_Earth_orbit
Amount by which an orbit deviates from a perfect circle
value of 0 is a circular orbit, values between 0 and 1 form an elliptic orbit, 1 is a parabolic (escape orbit or capture orbit), and greater than 1 is
Orbital_eccentricity
Type of spacecraft maneuver
a spacecraft to burn its fuel is at the lowest possible orbital periapsis, when its orbital velocity (and so, its kinetic energy) is greatest. In some
Oberth_effect
Term in geometry; longest and shortest semidiameters of an ellipse
eccentricity of the orbit. In astronomy, the semi-major axis is one of the most important orbital elements of an orbit, along with its orbital period. For Solar
Semi-major and semi-minor axes
Semi-major_and_semi-minor_axes
Geocentric orbit with an altitude entirely above that of a geosynchronous orbit
A high Earth orbit is a geocentric orbit with an apogee farther than that of the geosynchronous orbit, which is 35,786 km (22,236 mi) away from Earth.
High_Earth_orbit
Parameter in the gravitational two-body problem
two-body problem, the specific orbital energy ε {\displaystyle \varepsilon } (or specific vis-viva energy) of two orbiting bodies is the constant quotient
Specific_orbital_energy
Parameters that define a specific orbit
Kepler orbit. There are many different ways to mathematically describe the same orbit, but certain schemes are commonly used in astronomy and orbital mechanics
Orbital_elements
Type of orbit
mechanics a parabolic trajectory is a Kepler orbit with the eccentricity (e) equal to 1 and is an unbound orbit that is exactly on the border between elliptical
Parabolic_trajectory
The Moon's circuit around Earth
The orbit of the Moon is, while stable and known, highly complex, and as such still studied by lunar theory. Most models describe the Moon's orbit geocentrically
Orbit_of_the_Moon
Type of high-latitude satellite orbit
A Molniya orbit (Russian: Молния, IPA: [ˈmolnʲɪjə] , "Lightning") is a type of satellite orbit designed to provide communications and remote sensing coverage
Molniya_orbit
Satellite orbit with high inclination
A polar orbit is one in which a satellite passes above or nearly above both poles of the body being orbited (usually a planet such as the Earth, but possibly
Polar_orbit
maintain their orbit above a specific longitude, or to change longitude altogether. Spaceflight portal Orbital maneuver Hohmann transfer orbit Clohessy-Wiltshire
Orbit_phasing
Space navigation technique
gravitational slingshot in orbital mechanics, is a type of spaceflight flyby which makes use of the relative movement (e.g. orbit around the Sun) and gravity
Gravity_assist
Series of orbital maneuvers
into a lower orbit, which has a shorter orbital period allowing it to catch up, then executing a Hohmann transfer back to the original orbital height). As
Space_rendezvous
Motion problem in classical mechanics
used to calculate and predict the motion of two massive bodies that are orbiting each other in space. The problem assumes that the two bodies are perfect
Two-body_problem
Concept in celestial mechanics
is the minimum speed needed for an object to escape from contact with or orbit of a primary body, assuming: Ballistic trajectory – no other forces are
Escape_velocity
Angle between a reference plane and the plane of an orbit
Orbital inclination measures the tilt of an object's orbit around a celestial body. It is expressed as the angle between a reference plane and the orbital
Orbital_inclination
Application of mechanical dynamics to model the flight of space vehicles
the craft into the elliptical transfer orbit, and a second to circularize the target orbit. To raise a circular orbit at v 1 {\displaystyle v_{1}} ,
Spacecraft_flight_dynamics
Spaceflight where spacecraft orbits an astronomical body
An orbital spaceflight (or orbital flight) is a spaceflight in which a spacecraft is placed on a trajectory where it could remain in space for at least
Orbital_spaceflight
Circular orbit above Earth's Equator and following the direction of Earth's rotation
A geostationary orbit, also referred to as a GEO or GSO, is a circular geosynchronous orbit 35,786 km (22,236 mi) in altitude above Earth's equator, 42
Geostationary_orbit
Astrodynamic equation
In astrodynamics, an orbit equation defines the path of orbiting body m 2 {\displaystyle m_{2}\,\!} around central body m 1 {\displaystyle m_{1}\,\!}
Orbit_equation
Maintenance of a particular orbit
thruster burns to keep the active craft in the same orbit as its target. For many low Earth orbit satellites, the effects of non-Keplerian forces, i.e
Orbital_station-keeping
Center of mass of multiple bodies orbiting each other
(kéntron) 'center') is the center of mass around which two or more bodies orbit. A barycenter is a dynamical point, not a physical object. It is an important
Barycenter_(astronomy)
Either of two extreme points in a celestial object's orbit
nearest point in the orbit of a planetary body about its primary body. The line of apsides (also called apse line, or major axis of the orbit) is the line connecting
Apsis
2022 science fiction novel by Edward Ashton
while also putting a fresh spin on the idea of clones." Writing for Transfer Orbit, Andrew Liptak praised it as a "fun sci-fi romp, part Andy Weir's The
Mickey7
Problem in physics and celestial mechanics
predict a planet's motion; i.e., to give its orbital properties: position, orbital diameter, period and orbital velocity. Having done so, he and others soon
N-body_problem
Type of low-energy spacecraft transfer
spacecraft to achieve an orbit around a distant planet or moon with no fuel required to go into orbit. In the ideal case, the transfer is ballistic (requiring
Ballistic_capture
Point where an orbit crosses a plane of reference to which it is inclined
An orbital node is either of the two points where an orbiting object intersects a plane of reference inclined with respect to the orbital plane. A non-inclined
Orbital_node
Mathematical equation describing the motion of a rocket
applied to orbital maneuvers in order to determine how much propellant is needed to change to a particular new orbit, or to find the new orbit as the result
Tsiolkovsky_rocket_equation
Concept in astrodynamics
astrodynamics or celestial mechanics, a hyperbolic trajectory or hyperbolic orbit (from Newtonian theory: hyperbola shape) is the trajectory of any object
Hyperbolic_trajectory
Return of a spacecraft under gravity
In orbital mechanics, a free-return trajectory is a trajectory of a spacecraft traveling away from a primary body (for example, the Earth) where gravity
Free-return_trajectory
Horizontal angle from north or other reference cardinal direction
two-body orbits by eccentricity Circular orbit Elliptic orbit Transfer orbit (Hohmann transfer orbit Bi-elliptic transfer orbit) Parabolic orbit Hyperbolic
Azimuth
Characteristic of conic sections
close to the pericenter distance, the orbit is said to have low eccentricity; when they are very different, the orbit is said be eccentric or having eccentricity
Eccentricity_(mathematics)
Laws describing planetary orbits
astronomy, Kepler's laws of planetary motion give good approximations for the orbits of planets around the Sun. They were published by Johannes Kepler from 1608
Kepler's laws of planetary motion
Kepler's_laws_of_planetary_motion
typically carries the spacecraft to Geostationary Transfer Orbit, or GTO. From this elliptical orbit, the LEOP generally includes a sequence of apogee
Launch_and_Early_Orbit_phase
European heavy-lift space launch vehicle (1996–2023)
Guiana. It was used to deliver payloads into geostationary transfer orbit (GTO), low Earth orbit (LEO) or further into space. The launch vehicle had a streak
Ariane_5
Method to calculate trajectory calculations for spacecraft
made by assuming circular, coplanar planetary orbits and a Hohmann transfer orbit between the mean orbital radii of Earth and Mars. Let r E = 1.496 × 10
Patched_conic_approximation
Table of positions of astronomical objects at given times
include ephemeris data used to calculate the position of satellites in orbit. 1st millennium BC – Ephemerides in Babylonian astronomy. 2nd century AD
Ephemeris
Highly elliptical and highly inclined synchronous orbit
Tundra orbit (Russian: орбита «Тундра») is a highly elliptical geosynchronous orbit with a high inclination (approximately 63.4°), an orbital period of
Tundra_orbit
Classical approach to the many-body problem of astronomy
geometrical terms. This is called a two-body problem, or an unperturbed Keplerian orbit. The differences between that and the actual motion of the body are perturbations
Perturbation_(astronomy)
System for specifying positions of celestial objects
which include nutation. The fundamental plane is the plane of the Earth's orbit, called the ecliptic plane. There are two principal variants of the ecliptic
Astronomical coordinate systems
Astronomical_coordinate_systems
Russian heavy lift launcher which uses hypergolic fuel
Earth orbit. With an upper stage, it can place a 3000 kg payload into geostationary orbit (GEO), or a 5500 kg payload into geostationary transfer orbit (GTO)
Proton-M
launched to geostationary transfer orbit (GTO) was the 9,200 kg (20,300 lb) Jupiter-3 on July 29, 2023. Launches to higher orbits have included DSCOVR and
List of Falcon 9 and Falcon Heavy launches
List_of_Falcon_9_and_Falcon_Heavy_launches
Problem in celestial mechanics
mechanics, Lambert's problem is concerned with the determination of an orbit from two position vectors and the time of flight, posed in the 18th century
Lambert's_problem
Orbital perturbations
astronomy and astrodynamics the osculating orbit of an object in space at a given moment in time is the orbit it would have around its central body if perturbations
Osculating_orbit
archival service (link) "Launcher selects SpaceX for multiple launches of orbit transfer services". Launcher (Press release). 7 February 2022. Archived from
List of Falcon 9 and Falcon Heavy launches (2023)
List_of_Falcon_9_and_Falcon_Heavy_launches_(2023)
Proposed spacecraft in a closed transfer orbit between two celestial bodies
A cycler is a potential spacecraft on a closed transfer orbit that would pass close to two celestial bodies at regular intervals. Cyclers could be used
Cycler
Range of low orbital altitudes
Very low Earth orbit (VLEO) is a range of geocentric orbits with lowest altitudes (at perigee) below 400 km (250 mi). It is of increasing commercial importance
Very_low_Earth_orbit
American expendable launch system
placed NASA's Mars Observer spacecraft into heliocentric orbit, by means of a Transfer Orbit Stage. Wade, Mark. "Titan". Encyclopedia Astronautica. Archived
Commercial_Titan_III
Orbit around the planet Mars
orbit for an orbit around Earth and heliocentric orbit for an orbit around the Sun. As with these other orbits, the apsides of an areocentric orbit are
Areocentric_orbit
China crewed lunar surface lander
will transfer to the empty lander and proceed to attempt a landing on the lunar surface; the lander will return the astronauts to low lunar orbit after
Lanyue
Branch of astronomy
comets. Orbital mechanics focuses on spacecraft trajectories, including orbital maneuvers, orbital plane changes, and interplanetary transfers, and is
Celestial_mechanics
Orbital data format
three-line element set (3LE) is a data format encoding a list of orbital elements of an Earth-orbiting object for a given point in time, the epoch. Using a suitable
Two-line_element_set
Fifth planet from the Sun
the spacecraft, or delta-v. Entering a Hohmann transfer orbit from Earth to Jupiter from low Earth orbit requires a delta-v of 6.3 km/s, which is comparable
Jupiter
Branch of engineering
enter orbit around the Moon, with two, Neil Armstrong and Buzz Aldrin, visiting the lunar surface. The third astronaut, Michael Collins, stayed in orbit to
Aerospace_engineering
Celestial orbit whose trajectory is a conic section in the orbital plane
In celestial mechanics, a Kepler orbit (or Keplerian orbit, named after the German astronomer Johannes Kepler) is the motion of one body relative to another
Kepler_orbit
Proposed concepts
conjunction class, or the Crocco flyby. The lowest energy transfer to Mars is a Hohmann transfer orbit, a conjunction class mission which would involve a roughly
Human_mission_to_Mars
Physics algorithm
including low-energy transfer, is a concept introduced by Edward Belbruno in 1987. The concept explained how a spacecraft could change orbits using very little
Weak_stability_boundary
Time period during which a rocket must launch to reach its target
to another planet using the simple low-energy Hohmann transfer orbit, if eccentricity of orbits is not a factor, launch periods are periodic according
Launch_window
TRANSFER ORBIT
TRANSFER ORBIT
Boy/Male
African, American, Anglo, Australian, British, Chinese, English, French
Darling; Form of Daryl; Dear; Transfered Surname; Possibly Originated as a French Place Name; Like Darcy
Boy/Male
Muslim
Orbit, Eye socket, Argument
Boy/Male
Sikh
Battlefields protector
Boy/Male
Indian
Orbit, Eye socket, Argument
Surname or Lastname
English (mainly West Midlands)
English (mainly West Midlands) : occupational name for a peddler or hawker, especially one equipped with a horse and cart, Middle English traunter, traventer (Late Latin travetarius, of uncertain origin, possibly derived from Latin transvehere ‘to convey’).
Girl/Female
Bengali, Gujarati, Hindu, Indian, Kannada, Malayalam, Marathi, Telugu
Circumference of the Orbit; Limit; Realm
Boy/Male
Arabic, Hindu, Indian, Muslim, Sindhi
One who Argues a Lot; Orbit; Eye Socket; Orgument; Debate
Boy/Male
Indian, Punjabi, Sikh
The Lion of the Battlefield
Boy/Male
Muslim/Islamic
Orbit eye socket, Orgument, debate
Surname or Lastname
English
English : variant of Selman.North German (Sellmann) : topographic name from Middle Low German sele ‘meadow’, ‘bog’ + man ‘man’.South German : occupational name for a middleman in a land or property sale or for a guardian, from Middle High German sale ‘property transfer’.Jewish (Ashkenazic) : variant of Selman.
Boy/Male
African, American, Anglo, Australian, British, Chinese, Christian, English, French
Darling; Form of Daryl; Dear; Transfered Surname; Possibly Originated as a French Place Name; Like Darcy
Male
English
English occupational surname transferred to forename use, from a name for a "peddler, hawker," who drove a wagon, derived from the Middle English word traunter, TRANTER means "to convey."
Boy/Male
British, Christian, English
Wagoner; To Convey
TRANSFER ORBIT
TRANSFER ORBIT
Boy/Male
American, British, English
To Sing
Girl/Female
Muslim/Islamic
Good health
Male
English
Variant spelling of English Frederick, FREDRIC means "peaceful ruler."
Boy/Male
Hindu
Boy/Male
Arabic
Truth.
Girl/Female
British, English, Greek
Born of Zeus
Girl/Female
Indian
Charitable
Boy/Male
Hindu
Praised, Drawn, Described, Narrated
Male
French
French form or Roman Latin Maxentius, MAXENCE means "the greatest."
Boy/Male
Hindu, Indian, Traditional
Victory of Strength
TRANSFER ORBIT
TRANSFER ORBIT
TRANSFER ORBIT
TRANSFER ORBIT
TRANSFER ORBIT
v. t.
To change into another substance; to transmute; as, the alchemists sought to transform lead into gold.
n.
The conveyance of right, title, or property, either real or personal, from one person to another, whether by sale, by gift, or otherwise.
n.
Thin or transfer paper.
v. t.
To pierce through, as with a pointed weapon; to impale; as, to transfix one with a dart.
n.
A drawing or writing printed off from one surface on another, as in ceramics and in many decorative arts.
v. t.
To make over the possession or control of; to pass; to convey, as a right, from one person to another; to give; as, the title to land is transferred by deed.
n.
The person to whom a transfer in made.
n.
A pathological process by virtue of which a unilateral morbid condition on being abolished on one side of the body makes its appearance in the corresponding region upon the other side.
v. t.
To convey from one place or person another; to transport, remove, or cause to pass, to another place or person; as, to transfer the laws of one country to another; to transfer suspicion.
n.
A picture, or the like, removed from one body or ground to another, as from wood to canvas, or from one piece of canvas to another.
imp. & p. p.
of Transfer
p. pr. & vb. n.
of Transfer
n.
Mutual transfer; exchange.
n.
The act of transferring, or the state of being transferred; the removal or conveyance of a thing from one place or person to another.
v. t. & i.
To transmute; to transform; to metamorphose.
v. t.
To remove from one substance or surface to another; as, to transfer drawings or engravings to a lithographic stone.
v. t.
To transfer or transform the nature of.
v. t.
To transfer by draft.
n.
That which is transferred.
n.
A soldier removed from one troop, or body of troops, and placed in another.