Radial Position in Parabolic Orbit given Escape Velocity Calculator

✖Escape Velocity in Parabolic Orbit defined as the velocity needed for a body to escape from a gravitational center of attraction without undergoing any further acceleration.ⓘ Escape Velocity in Parabolic Orbit [v_p,esc]

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✖Radial Position in Parabolic Orbit refers to the distance of the satellite along the radial or straight-line direction connecting the satellite and the center of the body.ⓘ Radial Position in Parabolic Orbit given Escape Velocity [r_p]

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Radial Position in Parabolic Orbit given Escape Velocity Solution

STEP 0: Pre-Calculation Summary

Formula Used

Radial Position in Parabolic Orbit = (2*[GM.Earth])/Escape Velocity in Parabolic Orbit^2
r_p = (2*[GM.Earth])/v_p,esc^2
This formula uses 1 Constants, 2 Variables

Constants Used

[GM.Earth] - Earth’s Geocentric Gravitational Constant Value Taken As 3.986004418E+14

Variables Used

Radial Position in Parabolic Orbit - (Measured in Meter) - Radial Position in Parabolic Orbit refers to the distance of the satellite along the radial or straight-line direction connecting the satellite and the center of the body.
Escape Velocity in Parabolic Orbit - (Measured in Meter per Second) - Escape Velocity in Parabolic Orbit defined as the velocity needed for a body to escape from a gravitational center of attraction without undergoing any further acceleration.

STEP 1: Convert Input(s) to Base Unit

Escape Velocity in Parabolic Orbit: 5.826988 Kilometer per Second --> 5826.988 Meter per Second (Check conversion here)

STEP 2: Evaluate Formula

Substituting Input Values in Formula

r_p = (2*[GM.Earth])/v_p,esc^2 --> (2*[GM.Earth])/5826.988^2

Evaluating ... ...

r_p = 23478996.1152145

STEP 3: Convert Result to Output's Unit

23478996.1152145 Meter -->23478.9961152145 Kilometer (Check conversion here)

FINAL ANSWER

23478.9961152145 ≈ 23479 Kilometer <-- Radial Position in Parabolic Orbit

(Calculation completed in 00.020 seconds)

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Hindustan Institute of Technology and Science (HITS), Chennai, Indian

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< Parabolic Orbit Parameters Calculators

X Coordinate of Parabolic Trajectory given Parameter of Orbit

LaTeX Go X Coordinate Value = Parameter of Parabolic Orbit*(cos(True Anomaly in Parabolic Orbit)/(1+cos(True Anomaly in Parabolic Orbit)))

Y Coordinate of Parabolic Trajectory given Parameter of Orbit

LaTeX Go Y Coordinate Value = Parameter of Parabolic Orbit*sin(True Anomaly in Parabolic Orbit)/(1+cos(True Anomaly in Parabolic Orbit))

Escape Velocity given Radius of Parabolic Trajectory

LaTeX Go Escape Velocity in Parabolic Orbit = sqrt((2*[GM.Earth])/Radial Position in Parabolic Orbit)

Radial Position in Parabolic Orbit given Escape Velocity

LaTeX Go Radial Position in Parabolic Orbit = (2*[GM.Earth])/Escape Velocity in Parabolic Orbit^2

Radial Position in Parabolic Orbit given Escape Velocity Formula

LaTeX Go

Radial Position in Parabolic Orbit = (2*[GM.Earth])/Escape Velocity in Parabolic Orbit^2
r_p = (2*[GM.Earth])/v_p,esc^2

What is Radial Position in Parabolic orbit ?

In a parabolic orbit, the radial position refers to the distance from the focus (usually the center of the massive body being orbited) to the orbiting object at any given point along its trajectory.

How to Calculate Radial Position in Parabolic Orbit given Escape Velocity?

Radial Position in Parabolic Orbit given Escape Velocity calculator uses Radial Position in Parabolic Orbit = (2*[GM.Earth])/Escape Velocity in Parabolic Orbit^2 to calculate the Radial Position in Parabolic Orbit, The Radial Position in Parabolic Orbit given Escape Velocity is described by its distance from the focus of the orbit. Given the escape velocity, which is the minimum velocity required for an object to escape the gravitational pull of a massive body, we can derive the radial position at any point along the parabolic orbit. Radial Position in Parabolic Orbit is denoted by r_p symbol.

How to calculate Radial Position in Parabolic Orbit given Escape Velocity using this online calculator? To use this online calculator for Radial Position in Parabolic Orbit given Escape Velocity, enter Escape Velocity in Parabolic Orbit (v_p,esc) and hit the calculate button. Here is how the Radial Position in Parabolic Orbit given Escape Velocity calculation can be explained with given input values -> 23.53541 = (2*[GM.Earth])/5826.988^2.

FAQ

What is Radial Position in Parabolic Orbit given Escape Velocity?

The Radial Position in Parabolic Orbit given Escape Velocity is described by its distance from the focus of the orbit. Given the escape velocity, which is the minimum velocity required for an object to escape the gravitational pull of a massive body, we can derive the radial position at any point along the parabolic orbit and is represented as r_p = (2*[GM.Earth])/v_p,esc^2 or Radial Position in Parabolic Orbit = (2*[GM.Earth])/Escape Velocity in Parabolic Orbit^2. Escape Velocity in Parabolic Orbit defined as the velocity needed for a body to escape from a gravitational center of attraction without undergoing any further acceleration.

How to calculate Radial Position in Parabolic Orbit given Escape Velocity?

The Radial Position in Parabolic Orbit given Escape Velocity is described by its distance from the focus of the orbit. Given the escape velocity, which is the minimum velocity required for an object to escape the gravitational pull of a massive body, we can derive the radial position at any point along the parabolic orbit is calculated using Radial Position in Parabolic Orbit = (2*[GM.Earth])/Escape Velocity in Parabolic Orbit^2. To calculate Radial Position in Parabolic Orbit given Escape Velocity, you need Escape Velocity in Parabolic Orbit (v_p,esc). With our tool, you need to enter the respective value for Escape Velocity in Parabolic Orbit and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.

How many ways are there to calculate Radial Position in Parabolic Orbit?

In this formula, Radial Position in Parabolic Orbit uses Escape Velocity in Parabolic Orbit. We can use 1 other way(s) to calculate the same, which is/are as follows -

Radial Position in Parabolic Orbit = Angular Momentum of Parabolic Orbit^2/([GM.Earth]*(1+cos(True Anomaly in Parabolic Orbit)))

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