AI & ChatGPT searches , social queries for HOHMANN TRANSFER-ORBIT
Search references for HOHMANN TRANSFER-ORBIT. Phrases containing HOHMANN TRANSFER-ORBIT
See searches and references containing HOHMANN TRANSFER-ORBIT!
Search references for HOHMANN TRANSFER-ORBIT. Phrases containing HOHMANN TRANSFER-ORBIT
See searches and references containing HOHMANN TRANSFER-ORBIT!HOHMANN TRANSFER-ORBIT
Transfer manoeuvre between two orbits
In astronautics, the Hohmann transfer orbit (/ˈhoʊmən/) is an orbital maneuver used to transfer a spacecraft between two orbits of different altitudes
Hohmann_transfer_orbit
Elliptical orbit used to move a spacecraft from one circular orbit to another
geosynchronous transfer orbit is usually also a Hohmann transfer orbit Lunar transfer orbit is an orbit that touches Low Earth orbit and a lunar orbit. "Transfer Orbit"
Transfer_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
Transfer orbit used to reach geosynchronous or geostationary orbit
transfer orbit. In case of using the Hohmann transfer orbit, only a few days are required to reach the geosynchronous orbit. By using low-thrust engines or
Geostationary_transfer_orbit
Movement during spaceflight
elliptical orbit used to transfer between two circular orbits of different altitudes, in the same plane. The orbital maneuver to perform the Hohmann transfer uses
Orbital_maneuver
Type of orbital maneuver
transfer is an orbital maneuver that moves a spacecraft from one orbit to another and may, in certain situations, require less delta-v than a Hohmann
Bi-elliptic_transfer
German engineer
different orbits, now called a Hohmann transfer orbit. He received his Ph.D. from the RWTH Aachen University in 1920. Hohmann was born in Hardheim, the son
Walter_Hohmann
Orbit around the barycenter of the Sun
energy requirements. Transfer injections can place spacecraft into either a Hohmann transfer orbit or bi-elliptic transfer orbit. Trans-Mars injections
Heliocentric_orbit
altitude of a low Earth orbit (LEO) and the apogee at the altitude of a geostationary orbit. Hohmann transfer orbit: An orbital maneuver that moves a spacecraft
List_of_orbits
Type of low-energy spacecraft transfer
alternative to ballistic capture, spacecraft would either use a Hohmann transfer orbit or Oberth effect, which requires the spacecraft to burn fuel in
Ballistic_capture
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
Speed at which a body orbits around the barycenter of a system
interaction with a planet. Escape velocity Delta-v budget Hohmann transfer orbit Bi-elliptic transfer Lissauer, Jack J.; de Pater, Imke (2019). Fundamental
Orbital_speed
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
Fuel-efficient orbital maneuver
to complete than higher-energy (more-fuel) transfers, such as Hohmann transfer orbits. Low-energy transfers are also known as weak stability boundary trajectories
Low-energy_transfer
Field of classical mechanics concerned with the motion of spacecraft
transfer orbit requires a minimal delta-v. A bi-elliptic transfer can require less energy than the Hohmann transfer, if the ratio of orbits is 11.94 or
Orbital_mechanics
Spaceflight maneuver
[citation needed] For Hohmann transfer orbits, the initial orbit and the final orbit are 180 degrees apart. Because the transfer orbital plane has to include
Orbital_inclination_change
Topics referred to by the same term
Hohmann may refer to: Hohmann (surname) (article includes list of persons named Hohmann) Hohmann transfer orbit, in orbital mechanics Hohmann (crater)
Hohmann
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
Failed NASA mission to Mars (1998–1999)
into a Hohmann transfer orbit, sending the probe into a 9.5-month, 669 million km (416 million mi) trajectory. At launch, Mars Climate Orbiter weighed
Mars_Climate_Orbiter
Fifth planet from the Sun
of 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
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
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
Estimate of total change in velocity of a space mission
calculated with Hohmann transfer, which moves from one circular orbit to another coplanar circular orbit via an elliptical transfer orbit. In some cases
Delta-v_budget
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)
Propulsive maneuver used to arrive at the Moon
a fast Hohmann transfer is typically more practical. A spacecraft performs TLI to begin a lunar transfer from a low circular parking orbit around Earth
Trans-lunar_injection
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
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
maintain their orbit above a specific longitude, or to change longitude altogether. Spaceflight portal Orbital maneuver Hohmann transfer orbit Clohessy-Wiltshire
Orbit_phasing
Indian orbiter mission to Mars (2013–2022)
weather in the Pacific Ocean. Launch opportunities for a fuel-saving Hohmann transfer orbit occur every 26 months, in this case the next two would be in 2016
Mars_Orbiter_Mission
2015 space flight simulation video game
pseudorealistic orbital physics engine, allowing for various real-life orbital maneuvers such as Hohmann transfer orbits and orbital rendezvous. The first
Kerbal_Space_Program
Concept in gravitational orbital mechanics
the vis-viva equation is one of the equations that model the motion of orbiting bodies. It is the direct result of the principle of conservation of mechanical
Vis-viva_equation
Measure of amount of effort to change trajectory
changes due to gravity, e.g. in an elliptic orbit. For examples of calculating delta-v, see Hohmann transfer orbit, gravitational slingshot, and Interplanetary
Delta-v
Kind of planetary orbit
supersynchronous orbit is an orbit with a period greater than that of a synchronous orbit, or an orbit whose major axis is larger than that of a synchronous orbit. A
Supersynchronous_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
Orbit in the two body case with high eccentricity
the Polar regions. The transfer orbit was proposed by the German scientist Walter Hohmann in 1925, it connects two circular orbits, a lower one and a higher
Highly_elliptical_orbit
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
Crewed or uncrewed travel between stars or planets
meant using the Hohmann transfer orbit. Hohmann demonstrated that the lowest energy route between any two orbits is an elliptical "orbit" which forms a
Interplanetary_spaceflight
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
Application of mechanical dynamics to model the flight of space vehicles
several options: A Hohmann transfer orbit requires the least possible propellant and delta-v; this is half of an elliptical orbit with aphelion and perihelion
Spacecraft_flight_dynamics
Series of spacecraft designed for the Soviet space programme
travels on an elliptical Hohmann transfer orbit to the entry interface point, where atmospheric drag slows it enough to fall out of orbit. Early Soyuz spacecraft
Soyuz_(spacecraft)
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
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
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
Low-energy trajectories in the Solar System
lowest-energy transfers possible, even lower than the common Hohmann transfer orbit that has dominated orbital navigation since the start of space travel. Although
Interplanetary Transport Network
Interplanetary_Transport_Network
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
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
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
Rocket motor used to circularise a satellite's orbit after launch
motor was used to launch the New Horizons spacecraft towards Pluto. Hohmann transfer orbit Liquid apogee engine List of upper stages Advanced Cryogenic Evolved
Apogee_kick_motor
Orbit around Earth
than 1 whose orbit traces the path of an ellipse. Hohmann transfer orbit An orbital maneuver that moves a spacecraft from one circular orbit to another
Geocentric_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
Branch of astronomy
comets. Orbital mechanics focuses on spacecraft trajectories, including orbital maneuvers, orbital plane changes, and interplanetary transfers, and is
Celestial_mechanics
Either of two extreme points in a celestial object's orbit
apsides /ˈæpsɪˌdiːz/ AP-sih-deez) is one the two extreme points in the orbit of a planetary body about its primary body, either the farthest point (apoapsis)
Apsis
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
Topics referred to by the same term
station, in England High tibial osteotomy High Temperature Oxide Hohmann transfer orbit Holocene thermal optimum Waco HTO, an American biplane Partially
HTO
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)
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
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
Gravitational loss of momentum and energy by bodies moving through surrounding matter
stars causes matter to sink toward the center of the galaxy and for the orbits of stars to be randomized. This process is called violent relaxation and
Dynamical_friction
Return of a spacecraft under gravity
various trajectories to Mars for his mission design Mars Direct. The Hohmann transfer orbit can be made free-return. It takes 250 days (0.68 years) in the transit
Free-return_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
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
planet except Venus. Using a Hohmann transfer orbit, a trip to Mars requires approximately nine months in space. Modified transfer trajectories that cut the
Colonization_of_Mars
1990 Japanese lunar probe
lunar orbit using zero delta-v (called a ballistic transfer), but required five months instead of the usual three days for a Hohmann transfer orbit. This
Hiten_(spacecraft)
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
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
Property of a dynamical system where solutions near an equilibrium point remain so
principle Lyapunov–Malkin theorem Markus–Yamabe conjecture Libration point orbit Hartman–Grobman theorem Perturbation theory Stability theory Lyapunov, A
Lyapunov_stability
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 1609
Kepler's laws of planetary motion
Kepler's_laws_of_planetary_motion
Cancelled Canadian Mars lander and rover mission
orbital injection for a cruise vehicle that carries the Northern Light lander and the Beaver Rover to a direct rendezvous with Mars using a Hohmann transfer
Northern_Light_(spacecraft)
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
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
Earth-Mars-Venus-Earth route
though Walter Hohmann had already calculated the most energy-efficient trajectory between two similar circular orbits (the Hohmann transfer orbit) at the beginning
Crocco's Multiplanetary Trajectory
Crocco's_Multiplanetary_Trajectory
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
Region of space gravitationally dominated by a given body
hdl:11449/42361. ISSN 0035-8711. Seefelder, Wolfgang (2002). Lunar Transfer Orbits Utilizing Solar Perturbations and Ballistic Capture. Munich: Herbert
Sphere of influence (astrodynamics)
Sphere_of_influence_(astrodynamics)
Measure of the efficiency of a rocket based on its propellant's mass
two-body orbits by eccentricity Circular orbit Elliptic orbit Transfer orbit (Hohmann transfer orbit Bi-elliptic transfer orbit) Parabolic orbit Hyperbolic
Rocket_mass_ratio
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
Parameter of Keplerian orbits
parameter that defines the position of a body moving along a Keplerian orbit. It is the angle between the direction of periapsis and the current position
True_anomaly
Orbital mechanics term
In orbital mechanics, Kepler's equation relates various geometric properties of the orbit of a body subject to a central force. It was derived by Johannes
Kepler's_equation
Earliest phase of a flight that reaches space
atmosphere very early on, and then fly on for example, a Hohmann transfer orbit to reach the particular orbit that is required. This minimises the airdrag as well
Space_launch
Specifies the orbit of an object in space
the mean anomaly is the fraction of an elliptical orbit's period that has elapsed since the orbiting body passed periapsis, expressed as an angle which
Mean_anomaly
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
Method used to accelerate spacecraft
to move from one circular orbit to another is with a Hohmann transfer orbit: the spacecraft begins in a roughly circular orbit around the Sun. A short period
Spacecraft_propulsion
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
Measure of aircraft/spacecraft efficiency
considerably higher useful load fractions, on the order of 45–55%. For orbital rockets the payload fraction is between 1% and 5%, while the useful load
Payload_fraction
Time period during which a rocket must launch to reach its target
go 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
Concept in aerospace engineering
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
Propellant_mass_fraction
Specifies the orbit of an object in space
argument of pericenter), symbolized as ω (omega), is one of the orbital elements of an orbiting body. Parametrically, ω is the angle from the body's ascending
Argument_of_periapsis
Type of high-latitude satellite orbit
A Molniya orbit (Russian: Молния, IPA: [ˈmoɫnʲɪjə] , "Lightning") is a type of satellite orbit designed to provide communications and remote sensing coverage
Molniya_orbit
Region in which an astronomical body dominates the attraction of satellites
planet by a star, a moon by a planet—the less massive body must have an orbit that lies within the gravitational potential represented by the more massive
Hill_sphere
In astrodynamics and celestial mechanics a radial trajectory is a Kepler orbit with zero angular momentum. Two objects in a radial trajectory move directly
Radial_trajectory
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
Standard surface gravity
two-body orbits by eccentricity Circular orbit Elliptic orbit Transfer orbit (Hohmann transfer orbit Bi-elliptic transfer orbit) Parabolic orbit Hyperbolic
Surface_gravity
Chinese lunar exploration mission
from the lunar surface, the Orbiter and Returner successfully fired four engines to enter the Moon-Earth Hohmann transfer orbit. The electronics and systems
Chang'e_5
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
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
Spacecraft without people on board
along an orbit around the Sun similar to the Earth's orbit. To reach another planet, the simplest practical method is a Hohmann transfer orbit. More complex
Uncrewed_spacecraft
Type of engine
{\displaystyle \Delta v} from LEO is approximately 3000 m/s, using a Hohmann transfer orbit. For the sake of argument, assume the following thrusters are options
Reaction_engine
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
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
German American aerospace engineer (1912–1977)
using only one purely orbital cargo ship and one crewed craft. In each case, the expedition used minimum-energy Hohmann transfer orbits for its trips to Mars
Wernher_von_Braun
Guidance system — Hall-effect thruster — Heat shield — Helicopter — Hohmann transfer orbit — Hybrid rocket — Hydrodynamics — Hydrostatics — Hyperbolic partial
Index of aerospace engineering articles
Index_of_aerospace_engineering_articles
HOHMANN TRANSFER-ORBIT
HOHMANN TRANSFER-ORBIT
Boy/Male
Australian, Danish, Dutch, French, Swedish, Teutonic
Army Man; Soldier
Boy/Male
British, Christian, English
Wagoner; To Convey
Boy/Male
Indian
Good soul, Good natured
Boy/Male
Muslim
Good soul, Good natured
Surname or Lastname
Altered spelling of German Homann.English
Altered spelling of German Homann.English : variant of Holman. This surname has been in Ireland since the 17th century.Dutch : status name from Middle Dutch hovetman, hooftman ‘head man’, ‘leader’, ‘adviser’.Dutch : variant of Hoffman 2.Slovenian : unexplained.
Male
Danish
, man from the north, or, Niörd's man.
Boy/Male
German
Wealthy
Surname or Lastname
English (chiefly southern) and Dutch
English (chiefly southern) and Dutch : topographic name for a dweller in a hollow (see Hole).English (chiefly southern) : topographic name for a dweller by a holly tree or on an island, from Middle English holm (see Holme) + man.
Male
German
German name derived from Latin Johannes, JOHANN means "God is gracious."
Surname or Lastname
English
English : possibly a variant of Human.
Surname or Lastname
Altered spelling of German Luhmann or Lohmann.English
Altered spelling of German Luhmann or Lohmann.English : unexplained.
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’).
Surname or Lastname
English
English : variant of Human.
Boy/Male
Sikh
Battlefields protector
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
Teutonic Swedish
warrior.
Boy/Male
German
Hebrew John 'Jehovah has been gracious; has shown favor.
Boy/Male
Indian, Parsi
Good Nature; Having a Good Soul
Boy/Male
Indian, Punjabi, Sikh
The Lion of the Battlefield
Boy/Male
Australian, Danish, Dutch, Finnish, French, German, Hebrew, Slovenia, Swedish
God's Gracious Gift; The Lord is Gracious
HOHMANN TRANSFER-ORBIT
HOHMANN TRANSFER-ORBIT
HOHMANN TRANSFER-ORBIT
HOHMANN TRANSFER-ORBIT
HOHMANN TRANSFER-ORBIT
HOHMANN TRANSFER-ORBIT
HOHMANN TRANSFER-ORBIT
n.
The person to whom a transfer in made.
v. t.
To remove from one substance or surface to another; as, to transfer drawings or engravings to a lithographic stone.
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.
Thin or transfer paper.
v. t.
To pierce through, as with a pointed weapon; to impale; as, to transfix one with a dart.
pl.
of Hoyman
n.
Mutual transfer; exchange.
pl.
of Hodman
v. t. & i.
To transmute; to transform; to metamorphose.
n.
A drawing or writing printed off from one surface on another, as in ceramics and in many decorative arts.
n.
That which is transferred.
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.
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.
imp. & p. p.
of Transfer
v. t.
To transfer or transform the nature of.
n.
A soldier removed from one troop, or body of troops, and placed in another.
v. t.
To change into another substance; to transmute; as, the alchemists sought to transform lead into gold.
v. t.
To transfer by draft.
p. pr. & vb. n.
of Transfer