Notetaker: Electrical Power Subsystem Flashcards

1
Q

Identify

Generates, stores and distributes power throughout the spacecraft

Subsystem

A

Electrical Power Subsystem (EPS)

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2
Q

Identify

Most common source of power for earth orbit satellite

A

Solar Panels

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3
Q

What are the solar panel configurations?

A
  • Body Mounted
  • Sun Tracking
  • Roll Out
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4
Q

Identify

Simpler and more robust, but less effective at producing power

Solar Panel Configurations

A

Body Mounted

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5
Q

Identify

Not always within visibility of the sun; only capable of producing limited power for limited time

Solar Panel Configurations

A

Body Mounted

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6
Q

Identify

Effective for spin-stabilized satellites with lower power requirements

Solar Panel Configurations

A

Body Mounted

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7
Q

Identify

More complex than body mounted solars panels

Solar Panel Configurations

A

Sun Tracking

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8
Q

Identify

Provides higher level of power-to-weight efficiency, compared to body mounted

Solar Panel Configurations

A

Sun Tracking

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9
Q

Identify

Successfully tested 2017 on ISS, can be deployed and retracted

Solar Panel Configurations

A

Roll Out

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10
Q

Identify

20% lighter, 4x smaller, boost

Solar Panel Configurations

A

Roll Out

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11
Q

What are the Solar Panel Deployments?

A
  • Low Cycle
  • High Cycle
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12
Q

Identify

Exploding Bolts Solar Arrays

Solar Panel Deployment

A

Low Cycle

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13
Q

Identify

Deployed once and are never retracted (for sun-tracking solar panels)

Solar Panel Deployment

A

Low Cycle

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14
Q

Identify

Repeatable Deployment Solar Arrays

Solar Panel Deployment

A

High Cycle

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15
Q

Identify

High strain composite boom on both sides of solar arrays use stored energy, no motor, to change from a coil shape into a support arm

Solar Panel Deployment

A

High Cycle

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16
Q

Identify

Can use a motor to retract solar array

Solar Panel Deployment

A

High Cycle

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17
Q

Identify

Roll-out Solar Array

Solar Panel Deployment

A

High Cycle

18
Q

Identify

Solar cells produce most power when directly facing the sun; perpendicular to source of radiation

Solar Panel Operations

A

Incidence Angle

19
Q

Identify

Incidence angle and materials directly effect effectiveness of solar cells

Solar Panel Operations

A

Efficiency

20
Q

What are the two tasks of Solar Array Drive Mechanism (SADM)?

A
  • Positioning: Positions solar arrays to face the sun as directly as possible
  • Tracking: Constantly operate to track the sun while spacecraft maintains operational, earth-pointing attitude

Solar Array Drive Mechanism (SADM) is also “how to maintain it” in terms of solar panels.

21
Q

What are the two tasks of Sun Sensors?

A
  • Evaluation: Solar cells produce most power when directly facing the sun; perpendiculat to source of radiation
  • Determination: Incidence angle and materials directly affect effectiveness of solar cells

Sun Sensors are also “how to get feedback” in terms of solar panels.

22
Q

Identify

Supply power to components when needed

23
Q

Identify

Capable of more power than batteries wired in parallel

Battery Configuration

24
Q

Identify

If a single cell fails, the entire series of cells is nonfunctional

Battery Configuration

25
# Identify Hold a charge longer than batteries in series ## Footnote Battery Configuration
Parallel
26
# Identify Inherently redundant; failure of a single cell will not affect any other cells which require higher temperatures ## Footnote Battery Configuration
Parallel
27
# Identify First battery used in space ## Footnote Battery Cell Material
Nickel Cadmium (NiCd)
28
# Identify Large and susceptible to memory effect ## Footnote Battery Cell Material
Nickel Cadmium (NiCd)
29
# Identify Store a relatively small amount of power relative to mass and volume ## Footnote Battery Cell Material
Nickel Hydrogen (NiH2)
30
# Identify Solved the memory effect issue ## Footnote Battery Cell Material
Nickel Hydrogen (NiH2)
31
# Identify Not susceptible to memory effect ## Footnote Battery Cell Material
Lithium Ion (Li-ion)
32
# Identify Significantly lighter and more efficient than Nickel Hydrogen batteries ## Footnote Battery Cell Material
Lithium Ion (Li-ion)
33
# Identify Highly volatile and have the potential to explode if exposed to extreme heat or pressure ## Footnote Battery Cell Material
Lithium Ion (Li-ion)
34
# Identify During an eclipse: Solar arrays are unable to produce power, so batteries must be used to continue satellite operations ## Footnote Battery Use and Material
Operational Usage
35
# Identify When power demand is greater than generation: Batteries temporarily supplement until power load is decreased ## Footnote Battery Use and Material
Operational Usage
36
# Identify The life of battery is repeatedly overcharged, it builds up electrolyte crystals on the cathodes; results in lower discharge voltage ## Footnote Battery Use and Material
Voltage Depression
37
# Identify Combated by only charging the batteries when they need to be charged and stopping when they are fully charged ## Footnote Battery Use and Material
Voltage Depression
38
# Identify Mitigate effects of memory effect, voltage depression, and deep discharge ## Footnote Battery Use and Material
Reconditioning
39
# Identify Process of completely discharging then recharging ## Footnote Battery Use and Material
Reconditioning
40
What is responsible for allocating power in the correct voltages and current to the rest of the satellite?
Power Management Distribution (PMaD) System
41
What is the process of prioritizing components and shutting off power to less vital components?
Load Shedding