Planetary Environments Flashcards

1
Q

What is the surface gravity on the earth / moon / mars?

A

9,78, 1.62, 3.71 ms^-1

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2
Q

What is the rotation period of the earth / moon / mars?

A

23.93, 655.72, 24.62 sidereal hours

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3
Q

What is the average surface temperature on the earth / moon / mars?

A

185/331 , 26/396, 200/70 K

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4
Q

Does Mars / Moon have a global magnetic field?

A

No

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5
Q

What are the 7 main environmental factors?

A
  1. Vacuum
  2. Gravity
  3. Illumination
  4. Temperature
  5. Radiation
  6. Impacts
  7. Dust
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6
Q

What is Galilean invariance?

A

Gravitational acceleration is independent of objects mass

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7
Q

How does solar intensity vary with distance?

A

Inversely proportional to square of distance

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8
Q

What is the effect of the 14 day lunar day?

A
  • Limited Power
  • Reduced Radiation Intensity
  • Extreme Temperature Gradients
  • Psychological Effects
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8
Q

What is the formula for solar radiation?

A

q^dot = \sigma T^4 (R/r)^2

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9
Q

What are PEL and PSR’s

A

Peaks of eternal light and permanently shadowed regions

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10
Q

What are the sources of radiation?

A
  • High energy cosmic rays
  • Solar particle events
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11
Q

What are the effects of radiation?

A
  • DNA and cell damage –> Cataracts, gene mutations, increased chance of cancer, sterility
  • Jamming/damage of electronics –> Computer errors (glitches, bit flips, latchups, burnouts)
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12
Q

What are three philosophies of shielding electronics against radiation?

A
  • Radiation Hardening by architecture
  • Radiation Hardening by design
  • Radiation Hardening by process
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13
Q

What are some causes and consequences of impacts and why are they relevant?

A
  • Relevant because of lacking atmosphere on most celestial bodies, so no protection
  • Particle impact –> Mechanical damage, rupture, electrical failure
  • Secondary impacts –> Dust accumulation
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14
Q

What are the eight impact shielding concepts?

A
  • Monolithic (simple and heavy)
  • Whipple (thin bumper shocks the projectile, debris cloud less harmful)
  • Stuffed Whipple (variation of Whipple with layers of Nextel and Kevlar, further impact energy reduction)
  • Multi-Shock (staggered layers of Nextel)
  • Mesh Double Bumper (double layer bumper of aluminum mesh, aluminum rear wall)
  • Honeycomb Panel (light and rigid)
  • Foam Panel (light and rigid, better shielding than honeycomb)
  • Transhab (layers of Mylar, Nextel, Kevlar and foam, compressible for launch, prototype for Mars habitat)
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15
Q

What are some consequences of dust?

A
  • Inhalation of respirable fines –> Toxic, causes cancer
  • Skin exposure –> Allergic response (allergen unknown, might be nickel)
  • Abrasion and wear –> Decrease of lifetime
  • Particulate contamination –> Reduced seal tightness, clogging of moving parts, clouded solar cells
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16
Q

What are the natural sources of dust clouds?

A
  • Electrostatic transport, up to 300 g/m^2/a
  • Impact-generated dust, about 0.1 g/m^2/a
17
Q

What are the mitigation strategies for dust for spacecraft landing?

A

Landing pads
Surface Reinforcement
Berms

18
Q

What are some strategies for mitigating surface dust contamination?

A
  • Surface coatings that repel the dust
  • Removal of the dust
  • Altering the local lunar surface environment
  • Charged brushes
  • Systems that are designed to be tolerant of the dust
  • Redundant systems that use a combination of these approaches
  • Adjustment of operational procedures
19
Q

What is the ambient pressure at sea level of Earth, Moon and Mars?

A
  • Earth: 1013 mbar
  • Moon: 10^-11 to 10^-10 mbar
  • Mars: 6 mbar
20
Q

What are the effects and consequences of vacuum?

A
  • No oxygen –> life support system
  • Pressure difference –> pressure suit, reinforced structures
  • No convection –> highly variable thermal stress (sunlit planes/shadowed craters)
  • Material outgassing –> degradation, damage, contamination
  • No atmospheric drag –> meteoroid bombardment
21
Q

What happens to a human in space?

A
  • Air sucked out of lungs (holding breath causes tissue rupture)
  • Blood boils off
  • Other liquids boil off (Eyes, Tongue)
  • Local freezing
  • Ultimately full freezing, slower
22
Q

What are effects and consequences of reduced gravity?

A
  • Reduced contact to ground –> reduced traction and control, risk of bouncing off
  • Increased dust aggregation –> compromised vision, increased contamination
  • Varied fluid behaviour –> bubble growth/detachment and reduced convection (for reactors)
23
Q

What are effects and consequences of decreased illumination?

A
  • Limited power supply –> energy storage, other power sources
  • Reduced radiation intensity –> other power sources
  • Extreme temperature gradients –> thermal stress, damage, wide design envelope
  • Psychological effects –> psychological stress, mood
24
Q

Where can PEL’s and PSR’s be found and what are their benefits?

A
  • No evidence for “eternal light”, but peaks with illumination 80% of the time
  • Moon, Mercury, Ceres
  • Benefit: continuous power close to potential resource deposits
25
Q

What are effects and consequences of temperature?

A
  • Temporal/spatial gradients –> thermal stress (dynamic/static), thermal expansion
  • Extreme values –> enhanced outgassing, increased power demand
26
Q

What are some effects of Earth’s magnectic field?

A
  • Shields radiation
  • Traps highly energetic particles in the Van-Allen Belts
27
Q

Where are the 2 Van-Allen Belts located and where is a relatively safe zone?

A
  • Inner belt: 0.2 to 2 Earth radii, mainly protons
  • Outer belt: 3 to 10 Earth radii, protons and electrons with highest intensity around 4 to 5 Earth radii
  • Safe zone inbetween
28
Q

How much radiation dose is experienced on a trip to Mars compared to the recommended value for an average career?

29
Q

Can individual solar eruptions be forecasted and what is the time between an observation of an eruption and its arrival in the Earth-Moon system?

A
  • Impossible to forecast
  • Time between observation of an eruption and arrival in
    the Earth-Moon system is <1 h up to 4 h
30
Q

How many of the solar flares result in a particle event?

31
Q

What are some countermeasures against radiation exposure?

A
  • Timing of a mission
  • Careful planning of orbital trajectory
  • Shielding (Aluminum provides limited shielding, Propellant tanks much more efficient)
  • Risk of secondary radiation depending on material and thickness
  • Different materials for different types of radiation
32
Q

How can radiation hardening by architecture be achieved?

A
  • Redundancy (increases overhead in voting logic, power consumption, mass)
  • Multiple levels of redundancy (i.e. component, board, system, spacecraft level)
33
Q

How can radiation hardening by design be achieved?

A
  • Triple Modular Redundancy (TMR) strategies within the chip layout
  • Dopant wells and isolation trenches in the chip layout
  • Error detecting and correction circuits
  • Device spacing and decoupling
34
Q

How can radiation hardening by process be achieved?

A
  • Employ specific materials, processing techniques
  • Usually performed on dedicated rad-hard foundry fabrication lines
35
Q

What is triple modular redundancy?

A

Three systems perform a process and the result is processed by a majority-voting system to produce a single output

36
Q

How do radiation-hardened components and commercial components compare?

A

Radiation-hardened components lag behind commercial devices by several technology generations (~ 10 years)

37
Q

What is LUMIO and what is its purpose?

A
  • Newly approved CubeSat mission to observe meteoroid impacts on the lunar farside
  • Conduct observations of the lunar surface to detect impacts and characterise flux, magnitudes, luminous energies, sizes and locations
38
Q

What is an example of how larger structures could be protected from impacts and what are some aspects of this example?

A
  • Utilize caves or partially roofed-over rills
  • Protects from impacts, but also temperature gradients and radiation
  • Temperature inside lunar caves likely <200 K
  • 2 m layer could be stable over a 1 km wide tube
39
Q

How does dust differ on atmosphere-less bodies and bodies with atmosphere?

A
  • Atmosphere-less: Extremely fine grained, sharp-edged, adhesive
  • With atmosphere: Dust devils and sandstorms
40
Q

What is a general rule of thumb for solar array output decay?

A

~0.2% per Sol decay assuming no dust removal