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Aerospace Engineering
List of top Aerospace Engineering Questions on Space Dynamics
For an isentropic flow of a perfect gas, an increase in Mach number results in:
GATE AE - 2026
GATE AE
Aerospace Engineering
Space Dynamics
The velocity required for a satellite to remain in a circular orbit close to Earth is called:
GATE AE - 2026
GATE AE
Aerospace Engineering
Space Dynamics
The life of a geostationary communication satellite is limited by
TS PGECET - 2024
TS PGECET
Aerospace Engineering
Space Dynamics
To transfer a satellite from an elliptical orbit into a circular orbit having a radius equal to the apogee distance of the elliptical orbit, then the speed of the satellite should be
TS PGECET - 2024
TS PGECET
Aerospace Engineering
Space Dynamics
An artificial satellite remains in orbit and does not fall on to the Earth because
TS PGECET - 2024
TS PGECET
Aerospace Engineering
Space Dynamics
If the wind reference line coincides with the relative wind direction, then the axis system refers to
TS PGECET - 2024
TS PGECET
Aerospace Engineering
Space Dynamics