Two satellites of a planet have periods 32 days and 256 days. If the radius of orbit of former is R,find the orbital radius of the latter
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Answered by
55
Given : Time Period of 1st Satellite = 32 Days
Time period of 2nd Satellite = 256 Days
Radius of First Planet = R
Let Other satellite Be At a height of 'h' From 1st Satellite
We Know That Time Period T = 2π√(R/g)
Time Period Of First Satellite = T₁ = 2π√(R/g) = 32days
Time Period of Second Planet T₂ = 2π√[(R+h)]/g = 256days
T₁/T₂ = 32/256 = [2π√(R/g)] / [2π√[(R+h)]/g]
⇒1/8 = √(R)/(R+H)
⇒64 = (R+H)/R
⇒64 - 1 = H/R
⇒H = 63R
Orbital Raidius of Latter is 63R + R = 64R
∴ The Orbital Radius Of the Latter Satellite Is 64R
Time period of 2nd Satellite = 256 Days
Radius of First Planet = R
Let Other satellite Be At a height of 'h' From 1st Satellite
We Know That Time Period T = 2π√(R/g)
Time Period Of First Satellite = T₁ = 2π√(R/g) = 32days
Time Period of Second Planet T₂ = 2π√[(R+h)]/g = 256days
T₁/T₂ = 32/256 = [2π√(R/g)] / [2π√[(R+h)]/g]
⇒1/8 = √(R)/(R+H)
⇒64 = (R+H)/R
⇒64 - 1 = H/R
⇒H = 63R
Orbital Raidius of Latter is 63R + R = 64R
∴ The Orbital Radius Of the Latter Satellite Is 64R
Answered by
1
Answer:
4R
Explanation:
256 days ⇒ R = ?
Keplers 3ʳᵈ law ⇒
T²∝R³
(T₁/T₂)² = (R₁/R₂)³
(32/256)² = (R₁/R₂)³
(1/8)² = (R₁/R₂)³
1/64 = (R₁/R₂)³
1/4 ⇒ R₁/R₂
R₂ = 4R
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