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Orbital transfer From an Elliptical Initial Orbit

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Energy (Magnitude) of Initial orbit. Collected Equations: ... Energy (Magnitude) of Initial orbit. Burn 1 at Apogee. Burn 2 at Apogee (transfer orbit) ... – PowerPoint PPT presentation

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Title: Orbital transfer From an Elliptical Initial Orbit


1
Orbital transfer From an Elliptical Initial
Orbit
Vallado, Chapter 6, Sections 6.3.1, 6.3.2
2
QuestionWhere is the most fuelefficient place
to transfer from an initial elliptical orbitto a
final circular orbit?
3
Maximum Torque DV
4
DV Comparison
Case 1
Case 2
5
Burn 1 at Perigee
Final Orbit
Initial Orbit
Transfer Orbit
6
Compute DV1
7
Semi-Major Axisof transfer orbit
8
Substitute and Simplify

9
Substitute and Simplify (contd)
10
Normalized DV1 Working Formula
Energy (Magnitude) of Initial orbit
11
Burn 2 at Apogee
Final Orbit
Initial Orbit
Transfer Orbit
12
Compute DV2
13
Semi-Major Axisof transfer orbit
14
Substitute and Simplify
15
Continue Simplifying
16
Normalized DV2 Working Formula
Energy (Magnitude) of Initial orbit
17
Collected EquationsInitiate Transfer at Perigee
18
DV Comparison
Case 1
Case 2
19
Burn 1 at Apogee
Initial Orbit
Final Orbit
Transfer Orbit
20
Compute DV1 Burn 1 at Apogee
21
Normalized DV1 Working Formula
Energy (Magnitude) of Initial orbit
Burn 1 at Apogee
22
Burn 2 at Apogee (transfer orbit)
Final Orbit
Initial Orbit
Transfer Orbit
23
Compute DV2Burn 2 at Transfer Orbit Apogee
24
Semi-Major Axis of transfer orbit
All you need to do is ..
25
Normalized DV2 Working Formula
Energy (Magnitude) of Initial orbit
Burn 2 at Perigee
26
Collected EquationsInitiate Transfer at Apogee
27
Delta-V Plots
Initial
Effect of initial orbit Ellipticity
28
Delta-V Plots (contd)
Initial
For this example Final orbit is Circular thus
curves are monotonic
29
Rapogee a (1e)
30
(No Transcript)
31
Delta V ratio 2
32
Example Calculation
33
Comparative plot
Cheaper To transfer From apogee
34
Example Calculation (2)
35
Comparative Plot
36
Can We Exploit an InitialElliptical parking
Orbitto gain an advantage for transferring to a
Higher Final orbit?
37
Same Orbital Energies Different Velocities
38

???????????DV gains
Not much too to work with here .
39
???????????DV gains
40
Determines allowable Eccentricity on orbit For
a given average Altitude Zmin gt 80km
41
The Bottom Line
42
Something to Think About?
Can we exploit this region To design a transfer
maneuver that is more Efficient than a Hohmann
Transfer?
43
Answer Yes! Sometimes?
Next Time .. The Bi-elliptic transfer
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