5 RBTS PAPER(PHYSICS)
NEET Test Series from KOTA - 10 Papers In MS WORD WhatsApp Here
5 RBTS PAPER

164004 Select the incorrect statements from the following.
I. The orbital velocity of a satellite increases with the radius of the orbit
II. Escape velocity of a particle from the surface of the earth depends on the speed with which it is fired
III. The time period of a satellite does not depend on the radius of the orbit
IV. The orbital velocity is inversely proportional to the sequare root of the radius of the orbit.

1 I and II
2 I and IV
3 I, II and IV
4 I, II and III
5 RBTS PAPER

164005 Which of the following is/are not a relevant statement(s) to Kepler's laws of planetary motion?
I. Kepler's second law is based on law of conservation of angular momentum.
II. Every planet revolves around the sun in circular orbits with sun at the centre of the orbit.
III. Planets situated at larger distances from the sun take longer time to complete one rotation

1 I only
2 II only
3 II and III
4 I, II and III
5 RBTS PAPER

164006 Match the following :

A. Force between anyi. Maximum at the two bodies earth's surface
B. Acceleration due toii. Always attractive gravity
C. Escape velocityiii. \(\sqrt{\mathrm{gR}}\)
D. Orbital velocityiv. \(\sqrt{2} \cdot \sqrt{g R}\)

1 A-ii, B-i, C-iii, D-iv
2 A-i, B-ii, C-iv, D-iii
3 A-iv, B-iii, C-ii, D-i
4 A-ii, B-i, C-iv, D-iii
5 RBTS PAPER

164007 Match the following :

A. Potential energy of satellitei. Positive
B. Total energy of satelliteii. Negative
C. Kinetic energy of satelliteiii. Zero
D. Gravitational potential energy of satellite at infinityiv. Infinite

1 A-iv, B-ii, C-i, D-iii
2 A-iii, B-i, C-iv, D-ii
3 A-ii, B-ii, C-i, D-iii
4 A-ii, B-iv, C-i, D-iii
5 RBTS PAPER

164004 Select the incorrect statements from the following.
I. The orbital velocity of a satellite increases with the radius of the orbit
II. Escape velocity of a particle from the surface of the earth depends on the speed with which it is fired
III. The time period of a satellite does not depend on the radius of the orbit
IV. The orbital velocity is inversely proportional to the sequare root of the radius of the orbit.

1 I and II
2 I and IV
3 I, II and IV
4 I, II and III
5 RBTS PAPER

164005 Which of the following is/are not a relevant statement(s) to Kepler's laws of planetary motion?
I. Kepler's second law is based on law of conservation of angular momentum.
II. Every planet revolves around the sun in circular orbits with sun at the centre of the orbit.
III. Planets situated at larger distances from the sun take longer time to complete one rotation

1 I only
2 II only
3 II and III
4 I, II and III
5 RBTS PAPER

164006 Match the following :

A. Force between anyi. Maximum at the two bodies earth's surface
B. Acceleration due toii. Always attractive gravity
C. Escape velocityiii. \(\sqrt{\mathrm{gR}}\)
D. Orbital velocityiv. \(\sqrt{2} \cdot \sqrt{g R}\)

1 A-ii, B-i, C-iii, D-iv
2 A-i, B-ii, C-iv, D-iii
3 A-iv, B-iii, C-ii, D-i
4 A-ii, B-i, C-iv, D-iii
5 RBTS PAPER

164007 Match the following :

A. Potential energy of satellitei. Positive
B. Total energy of satelliteii. Negative
C. Kinetic energy of satelliteiii. Zero
D. Gravitational potential energy of satellite at infinityiv. Infinite

1 A-iv, B-ii, C-i, D-iii
2 A-iii, B-i, C-iv, D-ii
3 A-ii, B-ii, C-i, D-iii
4 A-ii, B-iv, C-i, D-iii
5 RBTS PAPER

164004 Select the incorrect statements from the following.
I. The orbital velocity of a satellite increases with the radius of the orbit
II. Escape velocity of a particle from the surface of the earth depends on the speed with which it is fired
III. The time period of a satellite does not depend on the radius of the orbit
IV. The orbital velocity is inversely proportional to the sequare root of the radius of the orbit.

1 I and II
2 I and IV
3 I, II and IV
4 I, II and III
5 RBTS PAPER

164005 Which of the following is/are not a relevant statement(s) to Kepler's laws of planetary motion?
I. Kepler's second law is based on law of conservation of angular momentum.
II. Every planet revolves around the sun in circular orbits with sun at the centre of the orbit.
III. Planets situated at larger distances from the sun take longer time to complete one rotation

1 I only
2 II only
3 II and III
4 I, II and III
5 RBTS PAPER

164006 Match the following :

A. Force between anyi. Maximum at the two bodies earth's surface
B. Acceleration due toii. Always attractive gravity
C. Escape velocityiii. \(\sqrt{\mathrm{gR}}\)
D. Orbital velocityiv. \(\sqrt{2} \cdot \sqrt{g R}\)

1 A-ii, B-i, C-iii, D-iv
2 A-i, B-ii, C-iv, D-iii
3 A-iv, B-iii, C-ii, D-i
4 A-ii, B-i, C-iv, D-iii
5 RBTS PAPER

164007 Match the following :

A. Potential energy of satellitei. Positive
B. Total energy of satelliteii. Negative
C. Kinetic energy of satelliteiii. Zero
D. Gravitational potential energy of satellite at infinityiv. Infinite

1 A-iv, B-ii, C-i, D-iii
2 A-iii, B-i, C-iv, D-ii
3 A-ii, B-ii, C-i, D-iii
4 A-ii, B-iv, C-i, D-iii
5 RBTS PAPER

164004 Select the incorrect statements from the following.
I. The orbital velocity of a satellite increases with the radius of the orbit
II. Escape velocity of a particle from the surface of the earth depends on the speed with which it is fired
III. The time period of a satellite does not depend on the radius of the orbit
IV. The orbital velocity is inversely proportional to the sequare root of the radius of the orbit.

1 I and II
2 I and IV
3 I, II and IV
4 I, II and III
5 RBTS PAPER

164005 Which of the following is/are not a relevant statement(s) to Kepler's laws of planetary motion?
I. Kepler's second law is based on law of conservation of angular momentum.
II. Every planet revolves around the sun in circular orbits with sun at the centre of the orbit.
III. Planets situated at larger distances from the sun take longer time to complete one rotation

1 I only
2 II only
3 II and III
4 I, II and III
5 RBTS PAPER

164006 Match the following :

A. Force between anyi. Maximum at the two bodies earth's surface
B. Acceleration due toii. Always attractive gravity
C. Escape velocityiii. \(\sqrt{\mathrm{gR}}\)
D. Orbital velocityiv. \(\sqrt{2} \cdot \sqrt{g R}\)

1 A-ii, B-i, C-iii, D-iv
2 A-i, B-ii, C-iv, D-iii
3 A-iv, B-iii, C-ii, D-i
4 A-ii, B-i, C-iv, D-iii
5 RBTS PAPER

164007 Match the following :

A. Potential energy of satellitei. Positive
B. Total energy of satelliteii. Negative
C. Kinetic energy of satelliteiii. Zero
D. Gravitational potential energy of satellite at infinityiv. Infinite

1 A-iv, B-ii, C-i, D-iii
2 A-iii, B-i, C-iv, D-ii
3 A-ii, B-ii, C-i, D-iii
4 A-ii, B-iv, C-i, D-iii