Physics Gravitation

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2 months ago

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A
Aadit Singh Uppal

Contributor-Level 10

The minus sign in the formula indicates that:

  • A gravitational force exists.
  • The satellite cannot leave the orbit by itself.
  • A minimum threshold of energy will be required to move the satellite from its existing orbit.

New answer posted

2 months ago

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R
Raj Pandey

Contributor-Level 9

According to kepler's third law of time period –

  ( T A T B ) 2 = ( r A r B ) 3 r A r B = 4 1 / 3  

r 4 3 = 4 r B 3  

New answer posted

2 months ago

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A
alok kumar singh

Contributor-Level 10

Kindly go through the solution 

New answer posted

2 months ago

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A
alok kumar singh

Contributor-Level 10

b = a 1 - e 2

d A d t = L 2 m

A T = L 2 m

T = 2 m A L = 2 m π a b L = 2 m π a 2 1 - e 2 L

New answer posted

2 months ago

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R
Raj Pandey

Contributor-Level 9

V in = G M 2 R [ 3 ( r R ) 2 ] ,

V s u r f a c e = G M R , V out = G M r

New answer posted

2 months ago

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V
Vishal Baghel

Contributor-Level 10

T = 2 π r 3 G M e

T B T A = 2 π G M e ( r B 3 / 2 r A 3 / 2 ) = 2 * 3 . 1 4 6 . 6 7 * 1 0 1 1 * 6 * 1 0 2 4 [ ( 8 * 1 0 6 ) 3 2 ( 7 * 1 0 6 ) 3 2 ]

New answer posted

2 months ago

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A
alok kumar singh

Contributor-Level 10

  1 2 m V a 2 G M m 2 x  

           =   1 2 m V a 2 4 G M m 4 x , V a = 2 3 G M x

ROC at point – B

R O C = V b 2 a = 2 G M 3 R * 1 4 G M ( 4 R ) 2 = 8 R 3

 

New answer posted

2 months ago

0 Follower 9 Views

V
Vishal Baghel

Contributor-Level 10

v = √ (GM/r) (orbital speed)
⇒ GM = v²r ⇒ (GM/R²) = (v²r/R²) ⇒ g = (v²r/R²)

New answer posted

2 months ago

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R
Raj Pandey

Contributor-Level 9

g = G M in   r 2  , where M in   = 0 r ? ρ 4 π x 2 d x

M in   = 4 π ρ 0 0 r ? ? 1 - x 3 R 3 x 2 d x = 4 π ρ 0 r 3 3 - r 6 6 R 3 g = 4 π G ρ 0 6 2 r - r 4 R 3

For g  to be maximum or minimum or constant d g d r = 0 2 - 4 r 3 R 3 = 0 r = R 2 1 / 3

 

New answer posted

2 months ago

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V
Vishal Baghel

Contributor-Level 10

Let the origin be at the CM of the particles, let the initial positions of the particles be x = a/2 and x = -a/2 and let the instantaneous positions of the particles be x = r and x = -r
Let the instantaneous velocity of each particle be v
Let the time after which the distance between the particles has reduced to a/2 be T
Then, for the particle that was initially at x = -a/2,
(Gm²/ (2r)²) = -m (vdv/dr) ⇒ (Gm/r²) = - (4vdv/dr) ⇒ -4∫vdv = Gm∫ (dr/r²)
[v is negative because the velocity is towards the –X direction]
dr/dt = -√ (Gm/2) (1/r - 2/a)¹? ²
⇒ ∫ (a/2)^ (a/4) (r/√ (a-2r)dr = -√ (Gm/2a) ∫? dt
⇒ ∫ (a/2)^ (a/4

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