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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

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