Part 1
Part 2
Part 3
Part 4
Part 5
100
F=ma
Weight
100
F=mv^2/r
Centripetal Force
100
F=ma
Newtons second law
100
V=2πr/T
Orbital Velocity
100
R^3/T^2=R^3/T^2
Keplers third law of Periods
200
V=√GM/r
Orbital Velocity of a satellite.
200
V=√2Gm/r
Escape Velocity
200
E=-Gm1m2/r
Gravitational Potential Energy
200
P=mv
Momentum
200
J=Ft
Impulse
300
F=1/2 Pv^2CA
Atmospheric drag
300
V=u V^2=U^2 Δx=ut
Horizontal Motion
300
E=GMm/2r
Kinetic Energy of a Satellite
300
V=u+at V^2=U^2+2aΔy Δy=Ut+1/2 at^2
Vertical Motion
300
g+a/g
g force
400
1/2 mv^2
Kinetic Energy
400
V=√GM (2/r-1/a)
Velocity of a satellite at any point along an elliptical path.
400
F=Gm1m2/r^2
Gravitational Force
400
r^3/T^2= GM/4π^2
the constant k
400
6.67x10-11
Gravitational Constant
500
tv=t0/√1-V^2/C^2
Time dilation.
500
Mv=M0/√1-V^2/C^2
Mass Dilation
500
5.97x10_24
Earths mass
500
Lv-L0√1-V^2/C^2
Length Contraction
500
6.378x10_6
Earths radius in metres
M
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