Home
Class 11
CHEMISTRY
The gaseous envelope around the earth is...

The gaseous envelope around the earth is known ias atmosphere. The lowest layer of this is extended upto `10` km from sea level , this layer is

A

stratosphere

B

troposphere

C

mesosphere

D

hydrosphere

Text Solution

AI Generated Solution

The correct Answer is:
To solve the question regarding the lowest layer of the atmosphere that extends up to 10 km from sea level, we can follow these steps: ### Step-by-Step Solution: 1. **Understanding the Atmosphere**: The atmosphere is the gaseous envelope surrounding the Earth. It consists of several layers, each with distinct characteristics. 2. **Identifying the Layers of the Atmosphere**: The atmosphere is divided into several layers: - **Troposphere**: Extends from the Earth's surface up to about 10 km. - **Stratosphere**: Extends from the top of the troposphere up to about 50 km. - **Mesosphere**: Extends from the top of the stratosphere up to about 80 km. - **Thermosphere**: Extends from the top of the mesosphere up to about 500 km. - **Exosphere**: Extends from the top of the thermosphere up to about 700 km. 3. **Determining the Lowest Layer**: Since the question specifies the lowest layer that extends up to 10 km from sea level, we identify that this layer is the **Troposphere**. 4. **Conclusion**: Therefore, the answer to the question is that the lowest layer of the atmosphere, which extends up to 10 km from sea level, is the **Troposphere**. ### Final Answer: The lowest layer of the atmosphere that extends up to 10 km from sea level is the **Troposphere**. ---
Promotional Banner

Topper's Solved these Questions

  • ENVIRONMENTAL CHEMISTRY

    NCERT FINGERTIPS ENGLISH|Exercise ASSERTION & REASON (CORNER)|15 Videos
  • ENVIRONMENTAL CHEMISTRY

    NCERT FINGERTIPS ENGLISH|Exercise Environment Pollution|1 Videos
  • ENVIRONMENTAL CHEMISTRY

    NCERT FINGERTIPS ENGLISH|Exercise HIGHHER ORDER THINKING SKILLS|9 Videos
  • CLASSIFICATION OF ELEMENTS AND PERIODICITY

    NCERT FINGERTIPS ENGLISH|Exercise Assertion And Reason|15 Videos
  • EQUILIBRIUM

    NCERT FINGERTIPS ENGLISH|Exercise Assertion And Reason|15 Videos

Similar Questions

Explore conceptually related problems

The gaseous envelope around the earth is known as atmosphere. The lowest layer of this is extended upto 10 km from sea level , this layer is

The layer of atmosphere which extends upto 10km from sea level is called

The layer of atmosphere between 10 km to 50 km above the sea level is called as:

What is the correct sequence of atmosphere layers starting from earth?

What is the correct sequence of atmosphere layers starting from earth?

An artificial satellite is orbiting around the earth with the speed of 4 km s^(-1) at a distance of 10^4 km from the earth. Calculate its centripetal acceleration.

Assertion : An equilibrium is established is istablished between generation and destruction of ozone, leading to a steady state concentration of ozone layer in the stratosphere at an altitude of 20-30 km above sea level. Reason : The thickness of the ozone layer is generally larger above the equator and smaller above the poles.

An artificial satellite is moving in a circular orbit around the earth with a speed equal to 3//8 times of th emagnitude of escape velocity from the earth. If the satellite is stopped suddely in its orbit and allowed to fall freely onto the earth, then the speed with whcih it hits the surface of the earth is (take g = 10 m//s and R_(e ) = 6400 km )

The moon takes about 27.3 days to revolve around the earth in a nearly circular orbit of radius 3.84xx10^5 km . Calculate the mass of the earth from these data.

Consider a spacecraft in an elliptical orbit around the earth At the lowest point or perigee of its orbit it is 300km above the earth's surface at the highest point or apogee it is 3000km above the earth surface (a) What is the period of the spacecraft's orbit (b) using conservation of angular momentum find the ratio of spacecraft's speed at perigee to its speed at apogee (c) Using conservation of energy find the speed at perigee and the speed at apogee (d) it is derised to have the spacecraft escape from the earth completrly if the spacecraft's rockets are fired at perigee by how much would the speed have to be increased to achieve this? What if the rockets were fired at apogee Which point in the orbit is the most efficient to use ?