00:47 485 32 4G 0 & 11 111.111 B/s V EXERCISE 3 A Delta IV launch vehicle delivers a Global Positioning System (GPS) satellite to a 185-km altitude circular low-Earth orbit (LEO). Determine the two Av impulses required for a coplanar Hohmann transfer to a 20,180-km altitude GPS circular orbit. In addition, compute the coast time for the Hohmann transfer to the target GPS orbit. Av₂ Av = 3.511 km/s T, 10, 604 5s = 2.95 h EVEDCICE A LEO Av, GPS orbit

Elements Of Electromagnetics
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ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
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00:47
485
32
4G
0 & 11 111.111
B/s
V
EXERCISE 3
A Delta IV launch vehicle delivers a Global Positioning System (GPS)
satellite to a 185-km altitude circular low-Earth orbit (LEO).
Determine the two Av impulses required for a coplanar Hohmann
transfer to a 20,180-km altitude GPS circular orbit. In addition,
compute the coast time for the Hohmann transfer to the target
GPS orbit.
Av₂
Av = 3.511 km/s
T, 10, 604 5s = 2.95 h
EVEDCICE A
LEO
Av,
GPS orbit
Transcribed Image Text:00:47 485 32 4G 0 & 11 111.111 B/s V EXERCISE 3 A Delta IV launch vehicle delivers a Global Positioning System (GPS) satellite to a 185-km altitude circular low-Earth orbit (LEO). Determine the two Av impulses required for a coplanar Hohmann transfer to a 20,180-km altitude GPS circular orbit. In addition, compute the coast time for the Hohmann transfer to the target GPS orbit. Av₂ Av = 3.511 km/s T, 10, 604 5s = 2.95 h EVEDCICE A LEO Av, GPS orbit
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