Flyby radius
WebNov 10, 2024 · Ganymede has a radius of 1,635 miles (2,631 kilometers) and is the largest moon in our solar system. It’s bigger than Mercury and Pluto. Ganymede is about 665,000 miles (1.07 million kilometers) from Jupiter, which orbits about 484 million miles (778 million kilometers) from the Sun. Jupiter is 5.2 astronomical units away from the Sun. WebCalculating the critical velocity (at which the flyby maneuver becomes more efficient) is straightforward, because it's the escape velocity, which is easy to calculate: v_esc = sqrt (GM/r_orbit) where r_orbit is the radius (not altitude) of the orbit.
Flyby radius
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WebThis applies to both a flyby mission and a rendezvous mission. All velocities in the solar system can be scaled to the orbital velocity of the Earth, Ve = 29.78 km s − 1, if the semimajor axis of the Earth is considered as the unit of distance (astronomical unit or AU). If Rp is the semimajor axis of the planet in these units, we have [4] WebRequiring the maneuver point to remain the periapsis of the capture orbit means that Δv is maximum for a circular capture orbit and decreases with increasing eccentricity until Δv = 0, which, of course, means no capture (flyby). In order to determine optimal capture radius, let us write Equation 8.60 in nondimensional form as (8.61) where (8.62)
WebMay 11, 2016 · From the measured ratio of luminosities, the radius of the hot companion must be in the range 0.1-0.5 Rsun (depending on the assumed radius of the red giant primary), which is an order of ... WebFor comparison, Pioneer 11 approached to 1.6 Jovian radii during its flyby in December 1974, and the Juno spacecraft is expected to orbit Jupiter with a periapse of approximately 1.07 Jovian radii ...
WebOver 16,000 potential Jupiter flyby trajectories were generated via the Program to Optimize Simulated Trajectories (POST). These trajectories were then input into the European Space Agency’s (ESA) Space Environment Information System (SPENVIS) to predict the total radiation dose behind 3 mm of Aluminum shielding. WebConsider a spacecraft on a hyperbolic trajectory that will fly by Mars. The trajectory's semi-major axis is -11,000km and it's eccentricity is 1.8. Calculate the turn angle, miss distance, hyperbolic excess speed, and radius of periapsis of …
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