Title: New Horizons
Content:  New Horizons has been called "the fastest spacecraft ever launched" because it left Earth at 16.26 km/s. It is also the first spacecraft launched directly into a solar escape trajectory, which requires an approximate speed while near Earth of 16.5 km/s, plus additional delta-v to cover air and gravity drag, all to be provided by the launch vehicle. However, it is not the fastest spacecraft to leave the Solar System. , this record is held by Voyager 1, traveling at 16.985 km/s relative to the Sun. Voyager 1 attained greater hyperbolic excess velocity than New Horizons due to gravity assists by Jupiter and Saturn. When New Horizons reaches the distance of 100 AU, it will be travelling at about 13 km/s, around 4 km/s slower than Voyager 1 
Title: New Horizons
Content:  that distance. The Parker Solar Probe can also be measured as the fastest object, because of its orbital speed relative to the Sun at perihelion: 95.3 km/s. Because it remains in solar orbit, its specific orbital energy relative to the Sun is lower than New Horizons and other artificial objects escaping the Solar System. New Horizons Star 48B third stage is also on a hyperbolic escape trajectory from the Solar System, and reached Jupiter before the New Horizons spacecraft; it was expected to cross Pluto's orbit on October 15, 2015. Because it was not in controlled flight, it did not receive the correct gravity assist, and passed within 200 e6km of Pluto. The Centaur second stage did not achieve solar escape velocity, and remains in a heliocentric orbit.
Title: Voyager program
Content:  spacecraft are headed now. This is the region where the Sun's influence begins to decrease and interstellar space can be detected. Voyager 1 is escaping the Solar System at the speed of 3.6 AU per year 35° north of the ecliptic in the general direction of the solar apex in Hercules, while Voyager 2s speed is about 3.3 AU per year, heading 48° south of the ecliptic. The Voyager spacecraft will eventually go on to the stars. In about 40,000 years, Voyager 1 will be within 1.6 light years (ly) of AC+79 3888, also known as Gliese 445, which is approaching the Sun. In 40,000 years Voyager 2 
Title: Characteristic energy
Content:  MAVEN, a Mars-bound spacecraft, was launched into a trajectory with a characteristic energy of 12.2 km2/s2 with respect to the Earth. When simplified to a two-body problem, this would mean the MAVEN escaped Earth on a hyperbolic trajectory slowly decreasing its speed towards. However, since the Sun's gravitational field is much stronger than Earth's, the two-body solution is insufficient. The characteristic energy with respect to Sun was negative, and MAVEN – instead of heading to infinity – entered an elliptical orbit around the Sun. But the maximal velocity on the new orbit could be approximated to 33.5 km/s by assuming that it reached practical "infinity" at 3.5 km/s and that such Earth-bound "infinity" also moves with Earth's orbital velocity of about 30 km/s. The InSight mission to Mars launched with a C3 of 8.19 km2/s2. The Parker Solar Probe (via Venus) plans a maximum C3 of 154 km2/s2. C3 (km2/s2) from Earth to get to various planets : Mars 12, Jupiter 80, Saturn or Uranus 147. To Pluto (with its orbital inclination) needs about 160–164 km2/s2.
Title: Elon Musk's Tesla Roadster
Content:  to leave Earth orbit, after the DSCOVR mission to the Earth–Sun Lagrangian point. Nine months after launch, the Tesla had travelled beyond the orbit of Mars, reaching aphelion at 12:48 UTC on November 9, 2018, at a distance of 248,892,559 km from the Sun. The maximum speed of the car relative to the Sun will be approximately 121,000 km/h at perihelion. Even if the rocket had targeted an actual Mars transfer orbit, the car could not have been placed into orbit around Mars, because the upper stage that carries it is not equipped with the necessary propellant, maneuvering, and communications capabilities. This flight simply demonstrated that Falcon Heavy is capable of launching significant payloads towards Mars in potential future missions.
Title: 2018 in spaceflight
Content: float = center ; width = 710 ; height = 400 ; stack = 1 ; group 1 = 23:0:0:0:0 ; group 2 = 13:0:0:0:0 ; group 3 = 30:0:0:0:0 ; group 4 =  1:0:0:0:0 ; group 5 = 0:13:0:0:0 ; group 6 = 0:0:27:0:0 ; group 7 = 0:0:0: 3:0 ; group 8 = 0:0:0:0: 4 colors = Navy : MediumBlue : RoyalBlue : DodgerBlue : LightSeaGreen : SaddleBrown : Black: Gold ; group names = Low Earth : Low Earth (ISS) : Low Earth (SSO) : Low Earth (retrograde) : Medium Earth :Geosychronous (transfer) : High Earth : Heliocentric ; x legends = Low Earth : Medium Earth : Geosynchronous / transfer : High Earth : Heliocentric orbit ; units suffix = _launches {{ #invoke:Chart | bar chart }}
Title: 343158 Marsyas
Content:  On 11 November 2024, Marsyas will pass about 0.485 AU from Earth, but with a record high relative velocity of about 283,000 km/h (78.66 km/s). Both Halley's Comet (254,000 km/h) and 55P/Tempel-Tuttle (252,800 km/h) have slightly lower relative velocities to Earth. Note however that when the asteroid is one astronomical unit from the sun (as it would be if it ever hit the earth), its relative speed will be less. On 2 February 2053, Marsyas will pass about 0.08 AU from Venus. On 22 October 2060, it may pass about 0.004 AU from Mars.
Title: Orbital mechanics
Content:  The formula for an escape velocity is derived as follows. The specific energy (energy per unit mass) of any space vehicle is composed of two components, the specific potential energy and the specific kinetic energy. The specific potential energy associated with a planet of mass M is given by The escape velocity from the Earth's surface is about 11 km/s, but that is insufficient to send the body an infinite distance because of the gravitational pull of the Sun. To escape the Solar System from a location at a distance from the Sun equal to the distance Sun–Earth, but not close to the Earth, requires around 42 km/s velocity, but there will be "partial credit" for the Earth's orbital velocity for spacecraft launched from Earth, if their further acceleration (due to the propulsion system) carries them in the same direction as Earth travels in its orbit.
Title: Escape velocity
Content:  In most situations it is impractical to achieve escape velocity almost instantly, because of the acceleration implied, and also because if there is an atmosphere, the hypersonic speeds involved (on Earth a speed of 11.2 km/s, or 40,320 km/h) would cause most objects to burn up due to aerodynamic heating or be torn apart by atmospheric drag. For an actual escape orbit, a spacecraft will accelerate steadily out of the atmosphere until it reaches the escape velocity appropriate for its altitude (which will be less than on the surface). In many cases, the spacecraft may be first placed in a parking orbit (e.g. a low Earth orbit at 160–2,000 km) and then accelerated to the escape velocity at that altitude, which will be slightly lower (about 11.0 km/s at 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 (in low Earth orbit speed is approximately 7.8 km/s, or 28,080 km/h).
Title: Escape velocity
Content:  In this table, the left-hand half gives the escape velocity from the visible surface (which may be gaseous as with Jupiter for example), relative to the centre of the planet or moon (that is, not relative to its moving surface). In the right-hand half, Ve refers to the speed relative to the central body (for example the sun), whereas Vte is the speed (at the visible surface of the smaller body) relative to the smaller body (planet or moon). The last two columns will depend precisely where in orbit escape velocity is reached, as the orbits are not exactly circular (particularly Mercury and Pluto).

Question: Verify the following claims with "True" or "False": The escape velocity of 58534 Logos is 0.02 km per sec and its apoapsis is 520906000.0 km.
Answer: False