A satellite in a circular orbit at altitude h above Earth's surface has period of revolution P. Compute (A) the speed, and (B) the centripetal acceleration, of the satellite. [ Data : h = 390 km; P = 92.26 minutes; ] %3D %3D Submit Answer Incorrect. Tries 4/12 Previous Tries Submit Answer Tries 0/12

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A satellite in a circular orbit at altitude h above
Earth's surface has period of revolution P. Compute
(A) the speed, and (B) the centripetal acceleration,
of the satellite.
[ Data : h = 390 km; P = 92.26 minutes; ]
%3D
%3D
Submit Answer
Incorrect. Tries 4/12 Previous Tries
Submit Answer Tries 0/12
Transcribed Image Text:A satellite in a circular orbit at altitude h above Earth's surface has period of revolution P. Compute (A) the speed, and (B) the centripetal acceleration, of the satellite. [ Data : h = 390 km; P = 92.26 minutes; ] %3D %3D Submit Answer Incorrect. Tries 4/12 Previous Tries Submit Answer Tries 0/12
Ang
iven
くこ 398 bn
Peñod P= 92.42 mimutes
= 92.42x60
と R+R
5545.2 8
ニ
= 6:37 XI8 + 0.398x18
6-768 XI8m
こ
Time pemod= my
レ
E
243.14x 6:768x10
レニ
P.
5545.2
42.50 3
3
メ10 ニ7664メ10切に
ニ
らこ4ら
レ= 7.664メ10 mg
Ceutripelal aecelesation
レ?
Qこ
(77664xる)
ニ
6.768X10
18.736X10
6.768 X10
ニ
8.678
a= 8.678 ml &?
Transcribed Image Text:Ang iven くこ 398 bn Peñod P= 92.42 mimutes = 92.42x60 と R+R 5545.2 8 ニ = 6:37 XI8 + 0.398x18 6-768 XI8m こ Time pemod= my レ E 243.14x 6:768x10 レニ P. 5545.2 42.50 3 3 メ10 ニ7664メ10切に ニ らこ4ら レ= 7.664メ10 mg Ceutripelal aecelesation レ? Qこ (77664xる) ニ 6.768X10 18.736X10 6.768 X10 ニ 8.678 a= 8.678 ml &?
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