Question: During a de-orbit burn, a pre-calculated V (delta V, change in velocity) will be used to decrease the Orion MPCV's altitude. The Orion MPCV's Orbital
During a de-orbit burn, a pre-calculated ∆V (delta V, change in velocity) will be used to decrease the Orion MPCV's altitude. The Orion MPCV's Orbital Maneuvering System (OMS) engines provide a combined thrust force of 53,000 Newtons. The Orion MPCV has a mass of 25,848 kg when fully loaded.
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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