हिंदी

A group of students from COEP Pune sent a small satellite _______ through ISRO in 2016.

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प्रश्न

A group of students from COEP Pune sent a small satellite _______ through ISRO in 2016.

विकल्प

  • Luna 6

  • Apollo 6

  • Swayam

  • Param

MCQ
रिक्त स्थान भरें
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उत्तर

A group of students from COEP Pune sent a small satellite Swayam through ISRO in 2016.

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  क्या इस प्रश्न या उत्तर में कोई त्रुटि है?
अध्याय 10: Space Missions - Choose the correct option.

संबंधित प्रश्न

Fill in the blank and explain the statement with reasoning:

 If the height of the orbit of a satellite from the earth surface is increased, the tangential velocity of the satellite will ...... 


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


Complete the following table.


If the height of a satellite completing one revolution around the earth in T seconds is h1 meter, then what would be the height of a satellite taking  \[2\sqrt{2} T\] seconds for one revolution?


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


Calculate the critical velocity of the satellite to be located at 35780 km above the surface of earth.


What is Medium Earth Orbit?


Distinguish between:

High Earth orbit - Medium Earth orbit.


Observe the figure and write the answers.

  1. Name the outer orbit.
  2. Which satellites revolve in low earth orbits?
  3. Which various orbits are given in the figure?
  4. Give an example of a launch vehicle based on Newton’s third law.

How is a satellite maintained in nearly circular orbit?


Why are some satellites called geostationary?


What is microgravity?


Give scientific reasons.

The geostationary satellite is not useful in the study of polar regions.


Geostationary satellites are not useful for studies of the polar region.


Calculate the time taken by a satellite for one revolution revolving at a height of 6400 km above the earth's surface with a velocity of 5.6 km/s.


The orbit of a satellite is exactly 35780 km above the earth's surface and its tangential velocity is 3.08 km/s.

How much time the satellite will take to complete one revolution around the earth?

(Radius of earth = 6400 km.)


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