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Introduction to Space Systems and Spacecraft Design

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Title: Introduction to Space Systems and Spacecraft Design


1
Power Systems Design -II
Introduction to Space Systems and Spacecraft
Design Space Systems Design
2
Power Systems Design II
Power Systems or EPS
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Introduction to Space Systems and Spacecraft
Design Space Systems Design
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Power Systems Design II
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Introduction to Space Systems and Spacecraft
Design Space Systems Design
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Power Systems Design II
Look at the parts of the EPS
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Introduction to Space Systems and Spacecraft
Design Space Systems Design
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Power Systems Design II
Take Solar Panel
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Introduction to Space Systems and Spacecraft
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Power Systems Design II
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Introduction to Space Systems and Spacecraft
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Power 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
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Power 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
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Power 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
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Power 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
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Power 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
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Rechargeable
Power Systems Design II
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Introduction to Space Systems and Spacecraft
Design Space Systems Design
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Power 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
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Power Systems Design II
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Introduction to Space Systems and Spacecraft
Design Space Systems Design
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Power 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
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Power 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
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Power 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
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Power Systems Design II
Packing Factor
Packing Factor Total Cell Area/ Total Panel Area
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Introduction to Space Systems and Spacecraft
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Packing 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
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Packing 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
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Power 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
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Power 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
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Power Systems Design II
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
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Power 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
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Power 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
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Power 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
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Power 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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Start here Tuesday for Idaho
Power Systems Design II
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Introduction to Space Systems and Spacecraft
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Power Systems Design II
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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Power Systems Design II
Power Systems or EPS
What is this?
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Introduction to Space Systems and Spacecraft
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Power 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
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Power 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
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Power Systems Design II
Power Systems or EPS
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Introduction to Space Systems and Spacecraft
Design Space Systems Design
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Power Systems Design II
Power Systems or EPS
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Introduction to Space Systems and Spacecraft
Design Space Systems Design
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Power Systems Design II
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Introduction to Space Systems and Spacecraft
Design Space Systems Design
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Power Systems Design II
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Introduction to Space Systems and Spacecraft
Design Space Systems Design
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Power Systems Design II
Expanded subsystem control
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Introduction to Space Systems and Spacecraft
Design Space Systems Design
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Power Systems Design II
Expanded subsystem control
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Introduction to Space Systems and Spacecraft
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Power 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
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Power Systems Design II
Expanded subsystem control
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Introduction to Space Systems and Spacecraft
Design Space Systems Design
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Power Systems Design II
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
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Power Systems Design II
Consider the satellites attitude control for
solar power generation.
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Introduction to Space Systems and Spacecraft
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Power Systems Design II
Satellite Orbit
Parallel Sun Rays
Eclipse
Sun
Earth
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Introduction to Space Systems and Spacecraft
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Gravity Gradient Stabilized
Power Systems Design II
Introduction to Space Systems and Spacecraft
Design Space Systems Design
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Passive Magnetic Stabilized
Power Systems Design II
N
S
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Introduction to Space Systems and Spacecraft
Design Space Systems Design
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Inertially Stabilized
Power Systems Design II
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Introduction to Space Systems and Spacecraft
Design Space Systems Design
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Power Systems Design II
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Introduction to Space Systems and Spacecraft
Design Space Systems Design
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Power Systems Design II
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Introduction to Space Systems and Spacecraft
Design Space Systems Design
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Power 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
    35

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Power Systems Design II
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Introduction to Space Systems and Spacecraft
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Power Systems Design II
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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Design Space Systems Design
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Power Systems Design II
Questions?
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Introduction to Space Systems and Spacecraft
Design Space Systems Design
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