During a de-orbit burn, a pre-calculated V (delta V, change in velocity) will be used to decrease
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2. Determination of ΔV (DeltaV): Find the change in altitude (Original Perigee - New Perigee) Use the conversion factor of (0.379[ms]/1km) . This conversion factor is the approximation of orbital velocity for the altitude difference, only valid for Earth's gravity and atmospheric drag for the altitudes of this problem.
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Fundamentals of Advanced Accounting
ISBN: 978-0077862237
6th edition
Authors: Joe Ben Hoyle, Thomas Schaefer, Timothy Doupnik
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