Explanation
Given that,
Acceleration a=2.45m/s2
Mass of earth M=6×1024kg
Radius of earth R=6×106m
Gravitational constant G=6.67×10−11Nm2/kg
Now centripetal acceleration is
ac=v2R
ac=(√GMR)2R
ac=GMR2
ac=GM(R+h)2
Now, put the values
2.45=6.67×10−11×6×1024(6×106+h)2
(6×106+h)2=6.67×10−11×6×10242.45
(6×106+h)2=40.02×10132.45
(6×106+h)2=1.6334×1014
6×106+h=√1.6334×1014
h=1.278×107−6×106
h=(12.78−6)×106
h=6.78×106
h=6.8×106m
So, h≅R
Hence, the height of spaceship is R
If t1 and t2 are the time when the body is at the same height Then h=12×g×t1×t2 h=12×g×2×10h = 10 g
So that the correct option is D
g=9.8m/s2
h=480km
R=6400km
We know that,
g′=g(1−2hR)
g′=9.8(1−2×4806400)
g′=8.33m/s2
Hence, the value of g’ is 8.33m/s2.
Net force on the rocket is zero. i.e. force due to the earth and force due to moon is same but in opposite direction.Fe=FmGMeMrre2=GMmMrrm2r is the total distancer=re+rmMe=81Mma81MmMrre2=GMmMrrm2rm=reggrm+rm=r⇒10rm=r⇒rm=r10
Weight of body W=144N
Height h=3R
Radius of earth =R
Acceleration due to gravity at the surface of the earth =g
Acceleration due to gravity at height g′=3R
Now,
gg′=(RR+h)2
gg′=(RR+3R)2
gg′=116
Now, weight at the height
w′w=mg′mg
w′w=116
w′=w16
w′=14416
w′=9N
Hence, the weight at the height is 9 N
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