6.17 A spacecraft is in a 300-km circular earth orbit. Calculate (a) The total delta-v required for the bielliptical transfer to the 3000-km-altitude coplanar circular orbit shown. (b) The total transfer time. {Ans.: (a) 2.039 km/s; (b) 2.86 h}

6.17 A spacecraft is in a 300-km circular earth orbit. Calculate (a) The total delta-v required for the bielliptical transfer to the 3000-km-altitude coplanar circular orbit shown. (b) The total transfer time. {Ans.: (a) 2.039 km/s; (b) 2.86 h}

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

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Question

6.17 A spacecraft is in a 300-km circular earth orbit. Calculate
(a) The total delta-v required for the bielliptical transfer to the 3000-km-altitude coplanar
circular orbit shown.
(b) The total transfer time.
{Ans.: (a) 2.039 km/s; (b) 2.86 h}
340
CHAPTER 6 ORBITAL MANEUVERS
e = 0.3
3000 km
300 km
AUA
CAUC
AUB

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