Solution.
a. r=1+0.6cosθ10000 ;
r=1+ecosθp;
e=0.6− the orbit is elliptical;
rp=1+ep;ra=1−ep;
rp=1+0.610000=6250;ra=1−0.610000=25000;
b. mb=5ma;
θb=θ;
mav0+0=mavacosθa+mbvbcosθb;
mav0=mavacosθa+5mavbcosθ;
vo=vacosθa+5vbcosθ; cosθa=vav0−5vbcosθ;
2mav02=2mava2+25mavb2;
v02=va2+5vb2;
c. x=0.02sin2π(t+0.01);
x=0.02sin(2πt+0.02π);
A=0.02m;
T=2π2π=1s;
vmax=ωA;
vmax=2π⋅0.02=0.04⋅3.14=0.1256m/s;
amax=ω2A;
amax=(2π)2⋅0.02=0.788m/s2;
xo=0.02sin0.02π=0.0012m;
Answer:a.e=0.6;rp=6250;ra=25000;
b. cosθa=vav0−5vbcosθ;
c.A=0.02m;T=1s;vmax=0.1256m/s;amax=0.788m/s2;x0=0.0012m.
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