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The critical speed of an artificial satellite is_______________?

Correct answer: C. 7.9 Kms-1

  • A. 8 Kms-1
  • B. 8.1 Kms-1
  • C. 7.9 Kms-1
  • D. 8 ms-1

Explanation

The speed needed for a low Earth satellite is v = √(GM/r), which gives approximately 7.9 km s-1 near Earth's surface. This speed provides the centripetal acceleration needed for circular orbit. Students may choose 8.1 km s-1 by using an over-rounded or slightly different orbital radius.

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