Turn Angle given Eccentricity Calculator

✖Eccentricity of Hyperbolic Orbit describes how much the orbit differs from a perfect circle, and this value typically falls between 1 and infinity.ⓘ Eccentricity of Hyperbolic Orbit [e_h]

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✖Turn Angle measures the change in direction or turning angle as the object travels through the hyperbolic path.ⓘ Turn Angle given Eccentricity [δ]

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Turn Angle given Eccentricity Solution

STEP 0: Pre-Calculation Summary

Formula Used

Turn Angle = 2*asin(1/Eccentricity of Hyperbolic Orbit)
δ = 2*asin(1/e_h)
This formula uses 2 Functions, 2 Variables

Functions Used

sin - Sine is a trigonometric function that describes the ratio of the length of the opposite side of a right triangle to the length of the hypotenuse., sin(Angle)
asin - The inverse sine function, is a trigonometric function that takes a ratio of two sides of a right triangle and outputs the angle opposite the side with the given ratio., asin(Number)

Variables Used

Turn Angle - (Measured in Radian) - Turn Angle measures the change in direction or turning angle as the object travels through the hyperbolic path.
Eccentricity of Hyperbolic Orbit - Eccentricity of Hyperbolic Orbit describes how much the orbit differs from a perfect circle, and this value typically falls between 1 and infinity.

STEP 1: Convert Input(s) to Base Unit

Eccentricity of Hyperbolic Orbit: 1.339 --> No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

δ = 2*asin(1/e_h) --> 2*asin(1/1.339)

Evaluating ... ...

δ = 1.68655278519253

STEP 3: Convert Result to Output's Unit

1.68655278519253 Radian -->96.6323565175845 Degree (Check conversion here)

FINAL ANSWER

96.6323565175845 ≈ 96.63236 Degree <-- Turn Angle

(Calculation completed in 00.004 seconds)

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Created by Harsh Raj

Indian Institute of Technology, Kharagpur (IIT KGP), West Bengal

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Indian Institute of Information Technology, Design And Manufacturing (IIITDM ), Jabalpur

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< Hperbolic Orbit Parameters Calculators

Radial Position in Hyperbolic Orbit given Angular Momentum, True Anomaly, and Eccentricity

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

Semi-Major Axis of Hyperbolic Orbit given Angular Momentum and Eccentricity

LaTeX Go Semi Major Axis of Hyperbolic Orbit = Angular Momentum of Hyperbolic Orbit^2/([GM.Earth]*(Eccentricity of Hyperbolic Orbit^2-1))

Perigee Radius of Hyperbolic Orbit given Angular Momentum and Eccentricity

LaTeX Go Perigee Radius = Angular Momentum of Hyperbolic Orbit^2/([GM.Earth]*(1+Eccentricity of Hyperbolic Orbit))

Turn Angle given Eccentricity

LaTeX Go Turn Angle = 2*asin(1/Eccentricity of Hyperbolic Orbit)

Turn Angle given Eccentricity Formula

LaTeX Go

Turn Angle = 2*asin(1/Eccentricity of Hyperbolic Orbit)
δ = 2*asin(1/e_h)

What is escape velocity ?

Escape velocity is the minimum velocity an object must have to break free from the gravitational attraction of a massive body without any additional propulsion. In simpler terms, it's the speed an object needs to reach to escape the gravitational pull of a planet, moon, or other celestial body and travel into space indefinitely.

How to Calculate Turn Angle given Eccentricity?

Turn Angle given Eccentricity calculator uses Turn Angle = 2*asin(1/Eccentricity of Hyperbolic Orbit) to calculate the Turn Angle, Turn Angle given Eccentricity formula is defined as a method to determine the angular displacement of an object in a hyperbolic orbit based on its eccentricity, which influences the trajectory and behavior of the orbiting body. Turn Angle is denoted by δ symbol.

How to calculate Turn Angle given Eccentricity using this online calculator? To use this online calculator for Turn Angle given Eccentricity, enter Eccentricity of Hyperbolic Orbit (e_h) and hit the calculate button. Here is how the Turn Angle given Eccentricity calculation can be explained with given input values -> 5536.626 = 2*asin(1/1.339).

FAQ

What is Turn Angle given Eccentricity?

Turn Angle given Eccentricity formula is defined as a method to determine the angular displacement of an object in a hyperbolic orbit based on its eccentricity, which influences the trajectory and behavior of the orbiting body and is represented as δ = 2*asin(1/e_h) or Turn Angle = 2*asin(1/Eccentricity of Hyperbolic Orbit). Eccentricity of Hyperbolic Orbit describes how much the orbit differs from a perfect circle, and this value typically falls between 1 and infinity.

How to calculate Turn Angle given Eccentricity?

Turn Angle given Eccentricity formula is defined as a method to determine the angular displacement of an object in a hyperbolic orbit based on its eccentricity, which influences the trajectory and behavior of the orbiting body is calculated using Turn Angle = 2*asin(1/Eccentricity of Hyperbolic Orbit). To calculate Turn Angle given Eccentricity, you need Eccentricity of Hyperbolic Orbit (e_h). With our tool, you need to enter the respective value for Eccentricity of Hyperbolic Orbit and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.

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