In orbital mechanics, low-thrust relative transfer is an orbital maneuver in which a chaser spacecraft covers a specific relative distance relative to...
7 KB (1,236 words) - 16:22, 4 October 2024
astronautics, the Hohmann transfer orbit (/ˈhoʊmən/) is an orbital maneuver used to transfer a spacecraft between two orbits of different altitudes around...
27 KB (3,626 words) - 18:17, 19 September 2024
orbital lifetime of the spent booster so as to curtail space junk. If using low-thrust engines such as electrical propulsion to get from the transfer...
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intended orbital changes using impulsive maneuvers that greatly reduces the complexity of finding the correct orbital transitions. Applying a low thrust over...
17 KB (2,128 words) - 07:32, 20 October 2024
low thrust. For the case of orbital transfer between non-coplanar orbits, the change-of-plane thrust must be made at the point where the orbital planes...
41 KB (5,821 words) - 22:06, 8 September 2024
}{2a}}\end{aligned}}} where v {\displaystyle v} is the relative orbital speed; r {\displaystyle r} is the orbital distance between the bodies; μ = G ( m 1 + m 2...
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Delta-v budget (section Earth–Moon space—low thrust)
propellant at low potential energy/high speed multiplies the effect of a burn. Thus for example the delta-v for a Hohmann transfer from Earth's orbital radius...
25 KB (2,727 words) - 05:46, 23 January 2024
astrodynamics, orbital station-keeping is keeping a spacecraft at a fixed distance from another spacecraft or celestial body. It requires a series of orbital maneuvers...
14 KB (1,757 words) - 14:36, 21 November 2024
acceleration to reach orbital speed. Higher energy orbits like geostationary orbit are often reached via elliptical transfer orbits. One type of orbit insertion is...
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Delta-v (section Orbital maneuvers)
notable that large thrust can reduce gravity drag. Delta-v is also required to keep satellites in orbit and is expended in propulsive orbital stationkeeping...
16 KB (2,194 words) - 15:23, 19 November 2024
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...
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Spaceflight (redirect from Difference between sub-orbital and orbital spaceflights)
which provide the thrust to overcome the force of gravity and propel spacecraft onto suborbital trajectories. If the mission is orbital, the spacecraft...
60 KB (6,987 words) - 18:44, 15 November 2024
elements. In some situations, description of orbital motion can be simplified and approximated by choosing orbital elements that are not osculating. Also,...
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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...
13 KB (1,968 words) - 18:02, 19 September 2024
The familiar study of jet aircraft treats jet thrust with a "black box" description which only looks at what goes into the jet engine, air and fuel, and...
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Mercury (planet) (redirect from Low-mass high-density planet)
angular orbital velocity equals its angular rotational velocity so that the Sun's apparent motion ceases; closer to perihelion, Mercury's angular orbital velocity...
155 KB (15,927 words) - 03:24, 22 November 2024
for a single-stage-to-orbit (SSTO) spaceplane, such heavy materials are unusable, and maximum thrust is necessary for orbital insertion at the earliest...
44 KB (4,564 words) - 19:39, 12 November 2024
BepiColombo (redirect from Mercury Magnetospheric Orbiter)
in an orbit similar to that of Mercury and will remain in the general vicinity of Mercury (see [1]). Four final thrust arcs reduce the relative velocity...
44 KB (3,728 words) - 07:52, 24 October 2024
Spacecraft propulsion (section Orbital)
direction), which increases/decreases altitude of orbit Perpendicular to orbital plane, which changes orbital inclination.[citation needed] Earth's surface...
91 KB (8,213 words) - 01:55, 28 September 2024
Gravity assist (redirect from Slingshot orbit)
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...
43 KB (4,953 words) - 16:56, 12 November 2024
the transfer orbit's departure speed and the departure planet's heliocentric orbital speed. Once this is determined, the injection velocity relative to...
47 KB (6,892 words) - 13:47, 4 October 2024
a very low perigee of 135 km, which is less than half the expected perigee altitude. [...] At this level of drag, our maximum available thrust is unlikely...
483 KB (19,992 words) - 00:20, 22 November 2024
Tsiolkovsky rocket equation (category Single-stage-to-orbit)
propagation of the spacecraft's state vector and the integration of thrust are used to predict orbital motion. Assume an exhaust velocity of 4,500 meters per second...
25 KB (4,354 words) - 07:21, 12 November 2024
Escape velocity (category Orbits)
a low Earth orbit of 200 km). The required additional change in speed, however, is far less because the spacecraft already has a significant orbital speed...
28 KB (3,658 words) - 17:32, 7 November 2024
high thrust, low specific impulse chemical rockets and low thrust, high specific impulse electric propulsion, but has not yet demonstrated high thrust. The...
30 KB (3,206 words) - 10:43, 14 July 2024
their thrusts being 40 and 83 mN, respectively. In the post-Soviet Russia high-power (a few kilowatts) SPT-140, SPT-160, SPT-200, T-160, and low-power...
40 KB (4,414 words) - 02:54, 11 November 2024
Space rendezvous (redirect from Orbital rendezvous)
match of the orbital velocities and position vectors of the two spacecraft, allowing them to remain at a constant distance through orbital station-keeping...
37 KB (3,811 words) - 00:46, 21 November 2024
choice whenever large amounts of thrust are needed and the cost is an issue. The Space Shuttle and many other orbital launch vehicles use solid-fueled...
28 KB (3,855 words) - 01:10, 7 October 2024
with 10 to 100 N of thrust have been investigated by SART. Reusable Orbital Transfer Vehicles (OTV), sometimes called (inter-orbital) space tugs, propelled...
13 KB (1,552 words) - 20:14, 22 August 2023
Starlink (redirect from Proliferated Low Earth Orbit program)
(340 mi) orbital altitude. These satellites would effectively operate in a third orbital shell, a 550 km (340 mi) orbit, while the higher and lower orbits at...
279 KB (23,706 words) - 16:59, 19 November 2024