$\dot{m} = C_d A \sqrt{\gamma \rho_0 P_0 ({2 \over {\gamma + 1}})^{{\gamma + 1} \over {\gamma -1}}}$
- $\dot{m}$ is the choked mass flow rate, the value we are looking for
- $C_d$ is the discharge coefficient. Let's go with 1.0 for space magic
- A is the area of the portal. A 5m diameter circular portal has an area of ~19.6 $m^2$
- $\gamma$ is the heat capacity ratio of the gas. For gaseous silicates we'll use 1.29
- $\rho_0$ is the gas density. We'll need to figure that out.
- $P_0$ is the upstream pressure. 30,000 atmospheres, or 3.045 gigapascals (GPa).
Calculating Density of Death World's Air
The equation for density is $ P = \rho R_{specific} T $
- P is 3.0 GPa ($3 \times 10^9$ Pa)
- T is 5,500 Kelvin
$R_{specific} = {R \over M}$
- R is the gas constant 8,314 ${m^2 kg} \over {s^{2} K mol}$
- M is molar mass. For silizate ($SiO_2$) gas, it's Si (28) + O (16) x 2 = 60 $g \over {mol}$
$R_{specific}$ = 138.6
$\rho_0$ = $P \over { R_{specific} T }$ = 3,995 $kg \over {m^3}$
Final Flow Rate
Inserting Variables and Solving :
- $\dot{m} = C_d A \sqrt{\gamma \rho_0 P_0 ({2 \over {\gamma + 1}})^{{\gamma + 1} \over {\gamma -1}}}$
- $\dot{m} = (1.0) (19.6) \sqrt{(1.29) (3,395) (3,045,000,000) ({2 \over {(1.29) + 1}})^{{(1.29) + 1} \over {(1.29) -1}}}$
- $\dot{m} = 19.6 \sqrt{(1.29) (3,395) (3,045,000,000) ({2 \over {2.29}})^{{2.29} \over {0.29}}}$
- $\dot{m} = 19.6 \sqrt{(1.29) (3,395) (3,045,000,000) (0.87)^{7.89}}$
- $\dot{m} = 19.6 \sqrt{(1.57 \times 10^{13}) (0.34)}$
- $\dot{m} = 19.6 \sqrt{5.34 \times 10^{12}}$
- $\dot{m} = (19.6) (5.34 \times 10^{6})$
- $\dot{m} = (4.53 \times 10^7)$ $kg \over s$
The average velocity of that gas is $\dot{m} = \rho v A$. Which is 577 $m \over s$.
Expansion and Cooling
After exiting the portal, the iron-laden silicate gas is expanding and cooling from 5,500 Kelvin and 30,000 atmospheres.
The speed of sound for this expanding death world gas is $a$ = $\sqrt{ \gamma R_{specific} T}$. $\gamma$ has a different meaning here. It's the adiabatic index, and for diatomic gasses it's 1.4 (not quite the tri-atomic SiO2; but using this for now). T is in Celsius instead of Kelvin.
- $a$ = $\sqrt{ (1.4) (138.6) (5,500) }$ = 1,032 $m \over s$
The death world gas is initially expanding from the portal at the it's speed of sound, 1,032 $m \over s$, or about Mach 3. Which would mean there's plenty of sound, noise, heat, and toxic vapor jetting out of this thing, but most of it is the higher-temperature, higher-pressure air expanding and cooling.
Limits
Where does the expansion end? ${P_1 V_1} \over {T_1}$ = ${P_2 V_2} \over {T_2}$. $P_1 \over P_2$ is 30,000. $T_1 \over T_2$ is ~ 200.
The volume at which the gas reaches Earth temperature and pressure $V_2 \over V_1$ should be 150 times the exit volume. For a portal 5 meters wide, I'd estimate you'd need a grid 750 meters on a side to keep people clear.
Heating
Some folks have asked about how much the portal to the death world starts to heat up the surrounding environment.
The heat passing through the portal is related to the mass flow rate, specific heat properties of the gas (glass), and the temperature difference between the portal and the environment
$\Delta Q = \dot{m} ( \Delta H_{vap} + \Delta H_{fus} + c \Delta T )$
- $\dot{m}$ was calculated above. $4.53 \times 10^7$ $kg \over s$
- $H_{vap}$ is 0 (according to this source)
- $H_{fus}$ is 0 (same source)
- c is 0.8 ${kJ} \over K$
- $\Delta T$ is (5,500K - 300K = 5,200K)
Solving:
- $\Delta Q = 4.53 \times 10^7 ( 0 + 0 + (0.8) (5,200) ) = 1.88 \times 10^{11}$ $J \over s$ = 188 $TJ \over s$
If I've done that right, $\Delta Q$ is 188 ${TJ} \over {s}$. Or 188 terawatts.
For scope, 80 terajoules is the amount of energy released by the first atomic bomb test.
Sound
Like the whistle of tea pot, or the rumble of an explosion, the portal will generate a sound that will carry for miles. I'd like the equation to figure out the frequency at the nozzle, but it escapes me at the moment.
Visibility
Iron and silicon dioxide (glass) are both solids at Earth pressures and temperatures. The cooling dome of gas would project nearly 1 kilometer up, and look something like the ash clouds over erupting volcanoes.
Survivability of a Probe
At 5,500 Kelvin, the atmosphere of the death world will even melt the most temperature-resistant material, Tungsten. Additionally, the ground beneath the gate is a gas at death-world temperatures. You shouldn't take it for granted that the gate is not now floating inside a crater of it's own making.
However, electronics that can survive the forces of being fired from a cannon are now a real thing.
The main gun of an M1A1 tank has a muzzle velocity of ~1,600 meters per second. From the safe zone, it could propel a saboted sensor package across the gap and into the gate in under half a second.
The sensor package would capture as much as it could before melting.
However, there's another problem. The cloud of iron and glass gas is an effective block to radio and optical signals for the probe to send back. Sonic is unlikely to be effective either. Thankfully, some nice fellows have invented neutrino communication, which can communicate through solid rock.
TL; DR
The portal would be incredibly hot, with an explosive blast spreading at Mach 3 from the portal area into the surroundings.