Space Propulsion - IAP/TU Wien
Space Propulsion - IAP/TU Wien
Space Propulsion - IAP/TU Wien
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<strong>Space</strong> <strong>Propulsion</strong><br />
Spiraling up<br />
dε<br />
=<br />
dt<br />
T<br />
v<br />
m<br />
=<br />
T<br />
v<br />
m<br />
at every moment, trajectories closely resemble circles (acc. to assumption T 0)<br />
v<br />
≅<br />
μ<br />
r<br />
ε ≅<br />
−<br />
μ<br />
2r<br />
ε = −<br />
μ<br />
2a<br />
dε<br />
dt<br />
dε<br />
dr<br />
= +<br />
dr dt<br />
=<br />
2<br />
μ dr<br />
2r<br />
dt<br />
=<br />
T<br />
v<br />
m<br />
≈<br />
μ T<br />
r m<br />
ΔV<br />
=<br />
t<br />
∫<br />
t0<br />
T<br />
m<br />
dt<br />
=<br />
r<br />
∫<br />
μ dr<br />
2 r<br />
= −<br />
μ.<br />
3/ 2<br />
r0 r r 0 0<br />
1<br />
r<br />
=<br />
μ<br />
−<br />
r<br />
μ<br />
r<br />
Δ<br />
V = v c , 0<br />
− v c , r<br />
thrusting ΔV is equal to difference<br />
of velocities in initial and final orbit