Title: Introduction to Space Systems and Spacecraft Design
1Power Systems Design -II
Introduction to Space Systems and Spacecraft
Design Space Systems Design
2Power Systems Design II
Power Systems or EPS
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Introduction to Space Systems and Spacecraft
Design Space Systems Design
3Power Systems Design II
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Introduction to Space Systems and Spacecraft
Design Space Systems Design
4Power Systems Design II
Look at the parts of the EPS
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Introduction to Space Systems and Spacecraft
Design Space Systems Design
5Power Systems Design II
Take Solar Panel
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Introduction to Space Systems and Spacecraft
Design Space Systems Design
6Power Systems Design II
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Introduction to Space Systems and Spacecraft
Design Space Systems Design
7Power Systems Design II
What do we need from the solar panel?
- What are the attributes of a solar panel?
- Total output power of solar panel.
- Voltage of solar panel.
- Maximum packing factor.
- Efficiency of the solar cells.
- Operating temperature of the panels.
Lets go back and look at the solar cell.
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Introduction to Space Systems and Spacecraft
Design Space Systems Design
8Power Systems Design II
Lets go back and look at the solar cell.
- This dual junction cell
- Has an efficiency of 22
- Open circuit voltage 2.2v
- Size 76 x 37 mm
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Introduction to Space Systems and Spacecraft
Design Space Systems Design
9Power Systems Design II
Solar cell has an I-V curve like this
- This dual junction cell
- Has an efficiency of 22
- Open circuit voltage 2.2v
- Size 76 x 37 mm
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Introduction to Space Systems and Spacecraft
Design Space Systems Design
10Power Systems Design II
- This dual junction cell
- Has an efficiency of 22
- Open circuit voltage 2.2v
- Size 76 x 37 mm
- What are the attributes of a solar panel?
- Total output power of solar panel.
- Voltage of solar panel.
- Maximum packing factor.
- Efficiency of the solar cells.
- Operating temperature of the panels.
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Introduction to Space Systems and Spacecraft
Design Space Systems Design
11Power Systems Design II
Need to select a battery to design for solar
panel voltage
- What are the attributes of a solar panel?
- Total output power of solar panel.
- Voltage of solar panel.
- Maximum packing factor.
- Efficiency of the solar cells.
- Operating temperature of the panels.
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Introduction to Space Systems and Spacecraft
Design Space Systems Design
12Rechargeable
Power Systems Design II
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Introduction to Space Systems and Spacecraft
Design Space Systems Design
13Power Systems Design II
Use a lithium ion battery
Li Ion batteries 3.6 v nominal
- Design Criteria for charging Li Ion battery
- Need 10-15 more voltage to charge than the
nominal voltage. - Here we would need solar panel voltage of 4.0
4.2v to charge this battery.
- Design Criteria solar panel
- Number of cells Max voltage/cell voltage.
- Take minimum number of whole cells.
- cells (4.2v/string)/(2.2v/cell)
- 1.9 or 2 cell for a string voltage
of 4.4v
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Introduction to Space Systems and Spacecraft
Design Space Systems Design
14Power Systems Design II
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Introduction to Space Systems and Spacecraft
Design Space Systems Design
15Power Systems Design II
Use two lithium ion batteries
Li Ion batteries 7.2 v nominal
- Design Criteria for charging Li Ion battery
- Need 10-15 more voltage to charge than the
nominal voltage. - Here we would need solar panel voltage of 8.0
8.3v to charge this battery.
- Design Criteria solar panel
- Number of cells Max voltage/cell voltage.
- Take minimum number of whole cells.
- cells (8.3v/string)/(2.2v/cell)
- 3.77 or 4 cell for a string voltage
of 8.8v - Lets be conservative and use 5 cells for 11v.
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Introduction to Space Systems and Spacecraft
Design Space Systems Design
16Power Systems Design II
Now we have
Two Li Ion batteries 7.2 v nominal
5 cells for 11v to charge with.
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Introduction to Space Systems and Spacecraft
Design Space Systems Design
17Power Systems Design II
What is packing factor?
- What are the attributes of a solar panel?
- Total output power of solar panel.
- Voltage of solar panel.
- Maximum packing factor.
- Efficiency of the solar cells.
- Operating temperature of the panels.
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Introduction to Space Systems and Spacecraft
Design Space Systems Design
18Power Systems Design II
Packing Factor
Packing Factor Total Cell Area/ Total Panel Area
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Introduction to Space Systems and Spacecraft
Design Space Systems Design
19Packing Factor
Power Systems Design II
Cell type 1
Cell type 2
Fixed solar panel size
Cell type 3
What do you do if given a fixed size panel on
which to put solar cells and you have these
different size solar cells?
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Introduction to Space Systems and Spacecraft
Design Space Systems Design
20Packing Factor
Power Systems Design II
What do you do if given a fixed size panel on
which to put solar cells and you have these
different size solar cells?
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Introduction to Space Systems and Spacecraft
Design Space Systems Design
21Power Systems Design II
Now we have
5 cells for 11v where the string has all of the
cells hooked in series
How do you mount these 5 cells on this panel?
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Introduction to Space Systems and Spacecraft
Design Space Systems Design
22Power Systems Design II
How do you mount these 5 cells on this panel?
OK!
NO!
Visually we can see a very poor packing factor.
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Introduction to Space Systems and Spacecraft
Design Space Systems Design
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What if the cells were bigger?
Oh Oh!
Now you have only 4.4v in the string.
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Introduction to Space Systems and Spacecraft
Design Space Systems Design
24Power Systems Design II
Got a cube? Put other cells on another face?
Cant do. All cells for a single string must be
on same face.
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Introduction to Space Systems and Spacecraft
Design Space Systems Design
25Power Systems Design II
Where are we now in the solar panel design?
- What are the attributes of a solar panel?
- Total output power of solar panel.
- Voltage of solar panel.
- Maximum packing factor.
- Efficiency of the solar cells.
- Operating temperature of the panels.
Got
Not got, but understand
Got
Assume we could mount the 5 cells on a panel,
what is total power for the cells selected?
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Introduction to Space Systems and Spacecraft
Design Space Systems Design
26Power Systems Design II
How much power from these cells?
5 cells for 11v
One cell area 76 x 37 mm 2812 mm2 Total cell
area 82812 22496 mm2 2.25 x10-2 m2 We
have 1350 watts/m2 from the sun in
space Direct power (1350 w/m2) x (2.25 x10-2
m2) 34.4
watts Converted power direct power x cell
efficiency 34.4 w x 0.22 eff 7.5
watts
11v
- For this dual junction cell
- Has an efficiency of 22
- Open circuit voltage 2.2v
- Size 76 x 37 mm
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Introduction to Space Systems and Spacecraft
Design Space Systems Design
27Power Systems Design II
Where are we now in the solar panel design?
- What are the attributes of a solar panel?
- Total output power of solar panel.
- Voltage of solar panel.
- Maximum packing factor.
- Efficiency of the solar cells.
- Operating temperature of the panels.
Got
Got
Not got, but understand
Got
- Now we can assume to start
- panel is at 90 degrees with sun max power
- operating temperature 20 degrees.. Centigrade
22 eff
Dont forget, temperature counts a lot.
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Introduction to Space Systems and Spacecraft
Design Space Systems Design
28Start here Tuesday for Idaho
Power Systems Design II
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Introduction to Space Systems and Spacecraft
Design Space Systems Design
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Now that we have beat our way through the solar
panel design ----- lets go look at the some more
parts of the EPS.
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Introduction to Space Systems and Spacecraft
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30Power Systems Design II
Power Systems or EPS
What is this?
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Introduction to Space Systems and Spacecraft
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31Power Systems Design II
Power Systems or EPS
Back bias diode
When panel 1 is shaded, the back bias diode keeps
the current from flowing backwards through panel
1, when panel 2 is generating a voltage across it.
Panel 1
Panel 2
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Introduction to Space Systems and Spacecraft
Design Space Systems Design
32Power Systems Design II
Power Systems or EPS
What is this?
R
V
Measure current by measuring voltage across a low
resistance precision resistor
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Introduction to Space Systems and Spacecraft
Design Space Systems Design
33Power Systems Design II
Power Systems or EPS
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Introduction to Space Systems and Spacecraft
Design Space Systems Design
34Power Systems Design II
Power Systems or EPS
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Introduction to Space Systems and Spacecraft
Design Space Systems Design
35Power Systems Design II
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Introduction to Space Systems and Spacecraft
Design Space Systems Design
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Introduction to Space Systems and Spacecraft
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37Power Systems Design II
Expanded subsystem control
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Introduction to Space Systems and Spacecraft
Design Space Systems Design
38Power Systems Design II
Expanded subsystem control
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Introduction to Space Systems and Spacecraft
Design Space Systems Design
39Power Systems Design II
- What does a charge regulator do?
- Controls voltage from PV to battery
- Controls rate of charge
- Prevents overcharging
- Can boost or buck PV voltage to match battery
needs.
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Introduction to Space Systems and Spacecraft
Design Space Systems Design
40Power Systems Design II
Expanded subsystem control
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Introduction to Space Systems and Spacecraft
Design Space Systems Design
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Consider When high current occurs in a
subsystem, it could be from latch-up. What to
do? Cycle power. Where do you do this
hardware controlled in the EPS.
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Introduction to Space Systems and Spacecraft
Design Space Systems Design
42Power Systems Design II
Consider the satellites attitude control for
solar power generation.
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Introduction to Space Systems and Spacecraft
Design Space Systems Design
43Power Systems Design II
Satellite Orbit
Parallel Sun Rays
Eclipse
Sun
Earth
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Introduction to Space Systems and Spacecraft
Design Space Systems Design
44Gravity Gradient Stabilized
Power Systems Design II
Introduction to Space Systems and Spacecraft
Design Space Systems Design
45Passive Magnetic Stabilized
Power Systems Design II
N
S
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Introduction to Space Systems and Spacecraft
Design Space Systems Design
46Inertially Stabilized
Power Systems Design II
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Introduction to Space Systems and Spacecraft
Design Space Systems Design
47Power Systems Design II
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Introduction to Space Systems and Spacecraft
Design Space Systems Design
48Power Systems Design II
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Introduction to Space Systems and Spacecraft
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49Power Systems Design II
Some Solar Notes
- Power from sun in orbit 1350 watts/meter2
- Power from cells on ground 35 less than in
space - Can get some power form albedo earth shine
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Introduction to Space Systems and Spacecraft
Design Space Systems Design
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Introduction to Space Systems and Spacecraft
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Need to consider the power requirements of all of
the subsystems and when they are used to build a
power budget.
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Introduction to Space Systems and Spacecraft
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52Power Systems Design II
Questions?
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Introduction to Space Systems and Spacecraft
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