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astrodynamics Meaning in kannada ( astrodynamics ಅದರರ್ಥ ಏನು?)



ಆಸ್ಟ್ರೋಡೈನಾಮಿಕ್ಸ್

ಖಗೋಳಶಾಸ್ತ್ರವು ಬಾಹ್ಯಾಕಾಶದಲ್ಲಿ ನೈಸರ್ಗಿಕ ಮತ್ತು ಕೃತಕ ಕಾಯಗಳ ಚಲನೆಯ ಅಧ್ಯಯನವಾಗಿದೆ,

astrodynamics ಕನ್ನಡದಲ್ಲಿ ಉದಾಹರಣೆ:

ಆಸ್ಟ್ರೋಡೈನಾಮಿಕ್ಸ್ - ಇದು ಗಗನ ನೌಕಾ ವಿಜ್ಞಾನದ ಅಧ್ಯಯನ ಶಾಖೆಯಾಗಿದ್ದು, ಇದು ಅಂತರಿಕ್ಷದಲ್ಲಿ ಚಲಿಸುವ ನೈಸರ್ಗಿಕ ಮತ್ತು ಕೃತಕ ವಾಹನಗಳ ಅಧ್ಯಯನವಾಗಿದೆ.

astrodynamics's Usage Examples:

astrodynamics, the orbital eccentricity of an astronomical object is a dimensionless parameter that determines the amount by which its orbit around another.


In astrodynamics, orbital station-keeping is keeping a spacecraft at a fixed distance from another spacecraft.


In astrodynamics, the characteristic energy ( C 3 {\displaystyle C_{3}} ) is a measure of the excess specific energy over that required to just barely.


In astronomy, and in particular in astrodynamics, the osculating orbit of an object in space at a given moment in time is the gravitational Kepler orbit.


Orbital mechanics or astrodynamics is the application of ballistics and celestial mechanics to the practical problems concerning the motion of rockets.


In astrodynamics or celestial mechanics, an elliptic orbit or elliptical orbit is a Kepler orbit with an eccentricity of less than 1; this includes the.


A sphere of influence (SOI) in astrodynamics and astronomy is the oblate-spheroid-shaped region around a celestial body where the primary gravitational.


In astrodynamics or celestial mechanics a parabolic trajectory is a Kepler orbit with the eccentricity equal to 1 and is an unbound orbit that is exactly.


Orbital mechanics or astrodynamics is the application of ballistics and celestial mechanics to the practical.


In astrodynamics and rocketry, gravity loss is a measure of the loss in the net performance of a rocket while it is thrusting in a gravitational field.


In astrodynamics or celestial mechanics, a hyperbolic trajectory is the trajectory of any object around a central body with more than enough speed to escape.


In astrodynamics the orbital period T of a small body orbiting a central body in a circular or elliptical orbit is: T 2 π a 3 μ , {\displaystyle.



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