A piece of debris is in circular Earth orbit at altitude 650 km. What is the speed of this orbit? (km/s) (b). What is the instantlaneous AV needed to slow the debris (I.o., by how much would you need to slow down the debris) so that it would be in an orbit of apogee altitude 650 km and perigee altitude 250 km? (km/s) Problem 6(a) ( An Earth orbit has perigee altitude 400 km and apogee altitudo 2000 km. What is the period of this orbit, in hours? (hours)

Elements Of Electromagnetics
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Author:Sadiku, Matthew N. O.
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Problem 5(a) (. s)
A piece of debris is in circular Earth orbit at altitude 650 km. What is the speed of this orblt?
(km/s)
(b),
What is the instanlaneous 4V needed to slow the debris (1.., by how much would you need to slow down
the debris) so that it would be in an orbit of apogee altitude 650 km and perigee altitude 250 km?
(km/s)
Problem 6(a) (
An Earth orbit has perigee altitude 400 km and apogee altitudo 2000 km. What is the period of this orbit, in
hours?
(hours)
(b)
When the vehicle is crossing altitude 1000 km, golng up (i.e., the altitude is increa: ng), what is the fight
path angle p, in degrees?
(degrees)
Transcribed Image Text:Problem 5(a) (. s) A piece of debris is in circular Earth orbit at altitude 650 km. What is the speed of this orblt? (km/s) (b), What is the instanlaneous 4V needed to slow the debris (1.., by how much would you need to slow down the debris) so that it would be in an orbit of apogee altitude 650 km and perigee altitude 250 km? (km/s) Problem 6(a) ( An Earth orbit has perigee altitude 400 km and apogee altitudo 2000 km. What is the period of this orbit, in hours? (hours) (b) When the vehicle is crossing altitude 1000 km, golng up (i.e., the altitude is increa: ng), what is the fight path angle p, in degrees? (degrees)
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