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The function of a satellite launcher is based on Newton's second law of motion. - Science and Technology 1

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प्रश्न

The function of a satellite launcher is based on Newton's second law of motion.

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उत्तर

The function of a satellite launcher is based on Newton's second law of motion- Wrong

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  क्या इस प्रश्न या उत्तर में कोई त्रुटि है?
अध्याय 10: Space Missions - Right or Wrong sentence

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संबंधित प्रश्न

Answer the question:

What is meant by the orbit of a satellite? On what basis and how are the orbits of artificial satellites classified?


Why are geostationary satellites not useful for studies of polar regions?


Solve the problem.

How much time a satellite in an orbit at height 35780 km above earth's surface would take, if the mass of the earth would have been four times its original mass?


Considering first correlation, complete the second.
Hubble telescope : At 569 km above the earth’s surface
Orbit of Hubble telescope : .............................


Mahendra and Virat are sitting at a distance of 1 metre from each other. Their masses are 75 kg and 80 kg respectively. What is the gravitational force between them? G = 6.67 x 10-11 Nm2/kg


Write the proper name of the orbits of satellites shown in the following figure with their height from the earth’s surface.


Name the first artificial satellite sent by Russia in space.


Distinguish between:

High Earth orbit - Medium Earth orbit.


Note the relationship between the entries in all the three columns in the table and rewrite the table.

Column-1
(Location)
Column-2
Height from the earth’s surface (km)
Column-3
g (m/s2)
Earth’s surface (average) 8.8 0.225
Mount Everest 36.6 9.81
Maximum height ever reached by manmade balloon 400 9.8
Orbit of a typical weather satellite 35700 9.77
Orbit of communication satellite 0 8.7

Define orbital velocity.


How is a satellite maintained in nearly circular orbit?


Why are some satellites called geostationary?


What is microgravity?


The orbital velocity of the satellite depends on its ______.


Write down the formula of orbital velocity.


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