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Transcription:

EART16: PLANETARY ATMOSPHERES Francis Nimmo

Last Week How do planets form? They accrete from the solar nebula (dust+gas) They may subsequently migrate Where do atmospheres come from? Primary, secondary, tertiary What observational constraints do we have on atmospheric properties? Radiometry/spectroscopy, occultations, in situ sampling Introduction to atmospheric structure Hydrostatic equilibrium, pressure scale height Exobase, tropopause 1 st homework due this Wednesday

Key equations Hydrostatic equilibrium: Ideal gas equation: P Scale height: H=RT/g dp dz RT ( z) g( z)

This Week Energy Budgets and Temperature Structures Energy Budgets Simplified temperature structures Solid planets Gas giants Radiative Transfer see next week Not going to treat entropy Taylor Ch.

1. Energy budgets

100% 76% reflected VENUS Solid Bodies 100% Note that Venus reflects more than 30% Earth! reflected EARTH 21% absorbed 3% at surface convection 100% 15% reflected MARS 20% absorbed 100% 50% at surface convection All absorbed energy is ultimately re-radiated at longer wavelengths 30% reflected TITAN convection 63% absorbed convection 85% at surface 7% at surface

T eq of an airless body What determines a planet s surface temperature? Incident energy Reflected energy Absorbed energy warms surface Energy re-radiated from warm surface 2 E in ( 1 A) R S R E R T rad 2 Sun A is Bond albedo, S is solar flux at planet s surface, is emissivity (usually=1), is Stefan s constant (5.67x10-8 Wm -2 K - ) Balancing energy in and energy out gives: T eq S (1 A) 1/ a

T eq calculations Venus Earth Mars Titan Solar constant S (Wm -2 ) 2620 1380 59 15.6 Bond albedo A 0.76 0. 0.15 0.3 T eq (K) 229 25 217 83 T surface or T 1bar (K) 730 288 220 95 T eq S (1 A) 1/ Greenhouse effect (K) 501 3 3 12 Calculation of T eq neglects any greenhouse effect (which can be significant) For bodies with thick atmospheres (e.g. Venus), T eq approximates the temperature at the cloud tops (clouds are opaque to long-wavelength radiation)

Greenhouse effect Atmosphere is more or less transparent to radiation (photons) depending on wavelength opacity Opacity is low at visible wavelengths, high at infra-red wavelengths due to absorbers like water vapour, CO 2 Incoming light (visible) passes through atmosphere with little absorption Outgoing light is infra-red (surface temperature is lower) and is absorbed by atmosphere So atmosphere heats up Venus suffered from a runaway greenhouse effect surface temperature got so high that carbonates in the crust dissociated to CO 2...

Albedo effects Fraction of energy reflected (not absorbed) by surface is given by the albedo A (0<A<1) Coal dust has a low albedo, ice a high one The albedo can have an important effect on surface temperature E.g. ice caps grow, albedo increases, more heat is reflected, surface temperature drops, ice caps grow further... runaway effect! This mechanism is thought to have led to the Proterozoic Snowball Earth How did the Snowball disappear? How did life survive? How might clouds affect planetary albedo?

Giant planet T eq Jupiter Saturn Uranus Neptune Solar constant S (Wm -2 ) 50.8 15.2 3.76 1.52 Bond albedo A 0.27 0.22 0.215 0.215 T eq (K) 113 8 60 8 T observed 127 96 59 60 Excess temperature (K) 1 12 (-1) 12 The excess temperatures are because the giant planets (except Uranus) are radiating internal heat as well as re-radiating the Sun s energy The excess temperature can be converted into an excess flux (e.g. 5.5 Wm -2 in Jupiter s case)

Gas Giants Incident solar radiation much less than that at Earth So surface temperatures are lower We can compare the amount of solar energy absorbed with that emitted. It turns out that there is usually an excess. Why? All units in W/m 2 8 incident 13.5 8.1 reflected.6 1 2.6 After Hubbard, in New Solar System (1999) Note that in some cases these numbers are quite uncertain! 3.5 1. 0.6 0.6 0.6 0.3 5. 2.0 0.3 Jupiter Saturn Uranus Neptune

Sources of Energy One major one is contraction gravitational energy converts to thermal energy. Helium sinking is another. Gravitational energy of a uniform sphere is 2 E g 0.6GM / So the rate of energy release during contraction is de g 0.6 2 dt GM R 2 R dr dt Where does this come from? e.g.jupiter is radiating 3.5x10 17 W in excess of incident solar radiation. This implies it is contracting at a rate of 0. km / million years Another possibility is tidal dissipation in the interior. This turns out to be small. Radioactive decay is a minor contributor.

Puzzles Why is Uranus heat budget so different? Perhaps due to compositional density differences inhibiting convection at levels deeper than ~0.6R p.may explain different abundances in HCN,CO between Uranus and Neptune atmospheres. Why is Uranus tilted on its side? Nobody really knows, but a possible explanation is an oblique impact with a large planetesimal (c.f. Earth-Moon) This impact might even help to explain the compositional gradients which (possibly) explain Uranus heat budget

2. Solid planet temperature structures

Adiabat Lower parts of most planetary atmospheres convect If a packet of gas rises rapidly (adiabatic), then it will expand and, as a result, cool We can balance the change in potential energy (per unit volume) against change in temperature: g dz This gives us the dry adiabatic lapse rate: dt g dz C p C p C p is the specific heat capacity of the gas at constant pressure is the mass of one mole, is the density of the gas At 1 bar level on Jupiter, T=165 K, g=23 ms -2, C p ~3R/, =0.002kg (H 2 ), so dt/dz = 1.8 K/km (adiabatic) dt

Moist adiabats In many cases, as an air parcel rises, some volatiles will condense out This condensation releases latent heat So the change in temperature with height is decreased compared to the dry case g dz C p dt L dx L is the latent heat (J/kg), dx is the incremental mass fraction condensing out C p ~ 1000 J/kg K for dry air on Earth dt dz g C p L The quantity dx/dt depends on the saturation curve and how much moisture is present (see Week ) E.g. Earth L=2.3 kj/kg and dx/dt~2x10 - K -1 (say) gives a moist adiabat of 6.5 K/km (cf. dry adiabat 10 K/km) dx dt

troposphere stratosphere Simplified Structure z Incoming photons (short l, not absorbed) thin Outgoing photons (long l, easily absorbed) Effective radiating surface T X adiabat Convection thick T X T s T Absorbed at surface

Key concepts are: 1) Input and output must balance at top of atmosphere 2) Atmosphere can radiate upwards and downwards T Balance at surface: eq Teq Simplified Structure (2) T s T eq Slab atmosphere Temperature T eq T eq T eq T s 2 1/ T eq 2T eq Surface T s Taylor pp. 9-96. This is a simplified argument which can be improved when we deal with radiative transfer (next week)

Simplified Structure (3) As before, for the stratosphere alone: 1) Input and output must balance 2) Stratosphere can radiate upwards and downwards z T eq slab stratosphere T X T X T T X X T X T T s T eq 1/ 2 X H T X dt dz eq adiabat H X T X dt dz T s T T s T X Convection T eq Note that now we are invoking convection, whereas in the previous slide we invoked radiative transfer...

Results T X T s 2 1/ T eq T X T s T eq 1/ 2 H X Solve for this dt dz Earth Mars T eq (K) 25 217 T X (K) 206 182 T s (K) 291 258 dt/dz (K/km) 10 2* H X (km) 8.5 38 Observed H X (appx.) 10 0 Quite good agreement (tends to underpredict T s and H X ) More sophisticated treatment requires radiative transfer (see later in course)

3. Gas giant deep & shallow structure

Gas Giants T eq T X 2T X T eq Fint slab stratosphere T X Convection F int T X Exactly the same picture as before Except here internal heat sources may also matter (see previous notes)

Giant planet atmospheric structure Tropospheric temperature gradient is adiabatic

Pressure Hydrostatic approximation ( r) g( r) dm( r) 2 Mass-density relation dr ( r) r These two can be combined (how?) to get the pressure at the centre of a uniform body P c : P c 3GM 8R Jupiter P c =7 Mbar, Saturn P c =1.3 Mbar, U/N P c =0.9 Mbar This expression is only approximate (why?) (estimated true central pressures are 70 Mbar, 2 Mbar, 7 Mbar) But it gives us a good idea of the orders of magnitude involved dp dr 2

Hydrogen phase diagram Jupiter interior mostly metallic hydrogen Saturn some metallic hydrogen Uranus/Neptune molecular hydrogen only Hydrogen undergoes a phase change at ~100 GPa to metallic hydrogen (conductive) It is also theorized that He may be insoluble in metallic H. This has implications for Saturn. Interior temperatures are adiabats

Compressibility & Density radius As mass increases, radius also increases But beyond a certain mass, radius decreases as mass increases. This is because the increasing pressure compresses the deeper material enough that the overall density increases faster than the mass Notice that S has more heavy elements (He) than J, and N more than U. So there are compositional variations. Also note that there are inflated hot Jupiter exoplanets which are larger than they should be why? mass

From Guillot, 200

More on the adiabat If no heat is exchanged, we have C p dt V dp Let s also define C p =C v +R and g=c p /C v A bit of work then yields an important result: g c P P ct g 1 or equivalently g Here c is a constant These equations are only true for adiabatic situations

Deep Temperature Structure At 1 bar level on Jupiter, T=165 K, g=23 ms -2, C p ~3R, =0.002kg (H 2 ), so dt/dz = 1.8 K/km (adiabatic) We can also use the expressions on the previous page to determine how temperature varies with pressure: T T 0 P P 0 g 1 g T 0 P P 0 R C p (Here T 0,P 0 are reference temp. and pressure) This is an example of adiabatic temperature and density profiles for the upper portion of Jupiter, using the same values as above, keeping g constant and assuming g=1.5 Note that density increases more rapidly than temperature why? Slope determined by g

Afterthought: molecular weight gradients We normally assume that gas giant interiors are well-mixed (because of convection). But, if there are molecular weight gradients, then convection can be reduced or stopped (why?) Less vigorous convection means smaller heat transfer. To keep the heat flux out of the top the same, we have to increase temperature gradients (to larger than adiabatic). Consequences: Heavy element abundance must increase Central temperatures increase Thermal timescales increase (initial conditions matter)

Solar constant, albedo Troposphere, stratosphere, tropopause Snowball Earth Adiabat, moist adiabat, lapse rate Greenhouse effect Metallic hydrogen Contractional heating Opacity Key concepts Hwk #2 due next Wednesday

End of lecture

Simplified Structure Incoming photons (short l) z thin Outgoing photons (long l) Convection Effective radiating surface T eff Most photons absorbed T eff T s T thick

Surface Temperature (2) Solar constant F E =1300 Wm -2 Earth (Bond) albedo A=0.29, =0.9 Equilibrium temperature = 263 K How reasonable is this value? T eq S (1 A) is Stefan s constant 5.67x10-8 in SI units 1/ Body Mercury Venus Earth Mars A 0.12 0.75 0.29 0.16 T eq 6 238 263 216 Actual T 100-725 733 288 222 How to explain the discrepancies? Has the Sun s energy stayed constant with time?

Adiabat Lower parts of most planetary atmospheres convect If a packet of gas rises rapidly (adiabatic), then it will expand and, as a result, cool Work done in expanding = work done in cooling VdP dp CpdT is the mass of one mole, is the density of the gas Combining these two equations with hydrostatic equilibrium, we get the dry adiabatic lapse rate: dt g dz a C p C p is the specific heat capacity of the gas at constant pressure At 1 bar level on Jupiter, T=165 K, g=23 ms -2, C p ~3R/, =0.002kg (H 2 ), so dt/dz = 1.8 K/km (adiabatic)

T X T 3 T s T eq 2 1/ H eq X Solve for this dt dz Results Earth Mars T eq (K) 25 217 T X (K) 206 182 dt/dz (K/km) 10 2* H X (km) 18 Observed H X (appx.) 10 0 T eq T eq slab atmosphere T eq T eq Earth Mars T s (K) 291 258 T X (K) 206 182 dt/dz (K/km) 10 2* H X (km) 8.5 38 Observed H X (appx.) 10 0 surface T s

Atmospheric Structure (2) Lower atmosphere (opaque) is dominantly heated from below and will be conductive or convective (adiabatic) Upper atmosphere intercepts solar radiation and re-radiates it There will be a temperature minimum where radiative cooling is most efficient; in giant planets, it occurs at ~0.1 bar Condensation of species will occur mainly in lower atmosphere mesosphere stratosphere tropopause radiation Temperature (schematic) ~0.1 bar Theoretical cloud distribution CH (U,N only) NH 3 80 K 10 K troposphere adiabat clouds NH 3 +H 2 S H 2 O 230 K 270 K