Question: During a de - orbit burn, a pre - calculated V ( delta V , change in velocity ) will be used to decrease the

During a de-orbit burn, a pre-calculated V (delta V, change in velocity) will be used to decrease the Orion MPCVs altitude. The Orion MPCVs 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.
What is the difference between the Orion MPCVs mass and weight? An objects mass does not change from place to place, but an objects weight does change as it moves to a place with a different gravitational potential. For example, an object on the moon has the same mass it had while on the Earth but the object will weigh less on the moon due to the moons decreased gravitational potential. The Orion MPCV always has the same mass but will weigh less while in orbit than it does while on Earths surface.
CALCULATION: Calculate how long a deorbit burn must last in seconds to achieve the Orion MPCV's change in altitude from 375.9 kilometers to 96.5 kilometers at
perigee. Use the equations and conversions provided to find the required burn time.
Equations to use:
Newton's Second Law F=ma
Where
a = acceleration is in meters per second per second (m/s^2) units
F= force is in Newtons 1N =1(k8-m/s^2)
M= mass is in ka units
Solve for a = F/m
2. Determination of AV (DeltaV):
Find the change in altitude (Original Perigee - New Perigee)
Use the conversion factor of (((0.379 m/s)/1km)
Equation should read AV (deltaV)=(Change in Altitude)0.379
3. Equation that defines average acceleration, the amount by which velocity will change in a given amount of time: a =deltaV/t
4. Rearrange the acceleration equation above to find the time required for a specific velocity change given a specific acceleration. where t =detlaV/a
AV(deltaV)= change in velocity in meters per second m/s
a = acceleration is in meters per second per second m/s^2
t= required time in seconds (this is the value you are solving for)

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