Question: During a de - orbit burn, a pre - calculated V ( delta V , change in velocity ) will be used to decrease the
During a deorbit burn, a precalculated 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 Newtons. The Orion MPCV has a mass of 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 MPCVs change in altitude from kilometers to kilometers at
perigee. Use the equations and conversions provided to find the required burn time.
Equations to use:
Newton's Second Law Fma
Where
a acceleration is in meters per second per second ms units
F force is in Newtons N kms
M mass is in ka units
Solve for a Fm
Determination of AV DeltaV:
Find the change in altitude Original Perigee New Perigee
Use the conversion factor of mskm
Equation should read AV deltaVChange in Altitude
Equation that defines average acceleration, the amount by which velocity will change in a given amount of time: a deltaVt
Rearrange the acceleration equation above to find the time required for a specific velocity change given a specific acceleration. where t detlaVa
AVdeltaV change in velocity in meters per second ms
a acceleration is in meters per second per second ms
t required time in seconds this is the value you are solving for
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