# Interstellar Medium Shielding

It might surprise you that you need to shield your ship from the interstellar medium, specifically at velocities greater than 40% of c. This is a result of interstellar space being filled with a diffuse medium of mostly hydrogen, which when relative to a ship at high enough velocities, comes to increasingly resemble ionizing radiation.

The main danger is heating and not erosion – erosion is insignificant enough that a 1 cm thick carbon shield can go 25,000 light-years (at a speed regime of 30% of c), ignoring that not all particles displaced will be lost to space, instead landing back on the shield.

# Interstellar Medium Density

To begin with, the interstellar medium density varies greatly, ranging from 10-4 particles per cubic centimeter in the coronal gas component of the galactic halo of the Milky Way, to 106 particles per cubic centimeter in molecular clouds. [1]

This is important in calculating the flux that the forward portion of the ship will receive at a particular velocity.

## Particle Density Table

(In units of particles per cubic centimeter)

Component Particle Density
Molecular clouds 102-106
H II regions 102-104
Cold neutral medium 20-50
Warm neutral medium 0.2-0.5
Warm ionized medium 0.2-0.5
Coronal gas
(Hot ionized medium)
10-4-10-2

The local neighborhood around the sun is assumed to have a particle density of 1 particle per cubic centimeter on average.

# Interstellar Medium Composition

By mass, the interstellar medium is 70% hydrogen, 28% helium and 2% heavier elements.
By number of atoms, the interstellar medium is 91% hydrogen, 8.9% helium and 0.1% heavier elements. [2]

There is also a dust component to the interstellar medium; the dust is considerably more dangerous than the diffuse gases as the particles are much larger. In the interstellar medium immediately around the Solar System, the mass of dust is ~0.5% of the mass of the gas, with the bulk of the particles ranging from 1E-18 to 1E-14 kg; however, the population of less-numerous but larger particles which pose the greatest hazard is not yet well known. [3]

# Erosion

Erosion is not taken to be a significant component of the danger in interstellar shielding. For example, at 30% of c a ship's forward shield will encounter 1E+18 ISM particles per square centimeter per light-year traveled (ignoring differences in ISM density through the journey).
A light year contains 946.1 quadrillion centimeters. In that length, there are thus 946.1 quadrillion cubic centimeters, and assuming a particle density of one per cubic centimeter, there are 9.467E+17 particles in that volume, rounding up to 1E+18.

If each impact displaces 2 atoms from the shield, every light year traveled will cause the loss of 2E+18 atoms per square centimeter. For carbon shields, this is a loss of 40 micrograms per light year per square centimeter, ignoring that not all particles displaced will be lost to space, instead landing back on the shield.

To get the mass loss rate, 2E+18 times the atomic mass of carbon gives 40 micrograms.

This means that a 1 cm thick shield, can survive a trip of 56,250 light-years before being worn through. At high relativistic velocities however, space-time contraction is significant enough that the effective ISM density increases.

The density of carbon, times the length, divided by mass loss rate gives the max trip length due to erosion.

Note: In the Daedalus report, a number of other mass loss factors and average of a variety of material choices gave a mass loss rate of 80 milligrams per cubic centimeter per light year at a speed of 25% of c. [4]

# Calculating the Heat Flux

Before we can begin calculating the flux, the mass density of the interstellar medium first be known.
The mass density is given by:

${\displaystyle \rho =mp}$

• where ${\displaystyle \rho }$ is the mass density of the interstellar medium
• where ${\displaystyle m}$ is the mass of the particle
• where ${\displaystyle p}$ is the particle density of the interstellar medium

Since the interstellar medium is not homogeneous, a weighted average must be done per the composition of the interstellar medium. We can assume that all of the heavier elements are iron atoms as an approximation.

${\displaystyle 1.475\cdot 10^{-27}kg\,(average\,\,mass)=(0.7\cdot H+0.28\cdot He+0.015\cdot Fe)/3}$

• ${\displaystyle H,\,\,He,\,\,Fe}$ respectively refer to the atomic masses of hydrogen, helium and iron.

Now we can finally calculate the flux with the relativistic flux equation [7]:

${\displaystyle \phi =\gamma \rho vc(\gamma -1)c^{2}}$

• where ${\displaystyle \phi }$ is the interstellar medium flux
• where ${\displaystyle \rho }$ is the mass density of the interstellar medium
• where ${\displaystyle v}$ is the velocity of the ship
• where ${\displaystyle c}$ is the speed of light
• where ${\displaystyle \gamma }$ is gamma, calculated with:
${\displaystyle \gamma =1/{\sqrt {1-v^{2}}}}$

Assuming a particle density of 1 particle per cubic centimeter, at 41% of the speed of light, the flux is comparable to what Earth receives from the sun, already enough for ice to begin melting. At 80% of the speed of the light, the flux is 35,327 W/m2.

# Calculating the Temperature of the Forward Shield

The temperature of the forward portion is given by the Stefan Boltzmann Law [5]:

${\displaystyle \phi _{e}=A_{d}\epsilon \sigma _{sb}T^{4}}$

• where ${\displaystyle \phi _{e}}$ is the radiant power
• where ${\displaystyle A_{d}}$ is the radiating/absorbing surface area
• where ${\displaystyle \epsilon }$ is the emissivity of the radiating/absorbing material
• where ${\displaystyle \sigma _{sb}}$ is the stefan boltzmann constant
• where ${\displaystyle T}$ is the temperature of the material

Now we rearrange the equation to solve for temperature:

${\displaystyle T={\sqrt[{4}]{\phi _{e}}}/({\sqrt[{4}]{A_{d}}}{\sqrt[{4}]{\epsilon }}{\sqrt[{4}]{\sigma _{sb}}})}$

Before we can solve the equation for temperature, the radiant power must be obtained from the interstellar medium flux, given by:

${\displaystyle \phi _{e}=IA}$

• where ${\displaystyle I}$ is the interstellar medium flux
• where ${\displaystyle A}$ is the area exposed to the interstellar medium flux

# Conclusions

A calculator for interstellar medium shielding is provided here:

Below are two tables:

## Velocity and Flux Table

(assuming particle density of 1 particle per cubic centimeter)

Ship Velocity Interstellar Medium
Heat Flux
0.1c 20.122 W/m2
0.2c 167.283 W/m2
0.3c 603.483 W/m2
0.4c 1579.947 W/m2
0.5c 3549.648 W/m2
0.6c 7451.7 W/m2
0.7c 15,593.049 W/m2
0.8c 35,326.58 W/m2
0.9c 106,195.696 W/m2
0.99c 1,698,225.484 W/m2
0.999c 18,973,260.691 W/m2

## Example Shield Temperature Table

Assuming a cylindrical shape, radius of 10 meters and thickness of 1 meter

Ship Velocity Interstellar Medium
Heat Flux
Ice
Temperature
Graphite
Temperature
0.1c 20.122 W/m2 113.558 K 123.207 K
0.2c 167.283 W/m2 192.824 K
Beyond
sublimation point [6]
209.208 K
0.3c 603.483 W/m2 265.744 K 288.325 K
0.4c 1579.947 W/m2 338.033 K
Too hot even at
standard pressure
366.756 K
0.5c 3549.648 W/m2 449.017 K
0.6c 7451.7 W/2 540.481 K
0.7c 15,593.049 W/m2 650.054 K
0.8c 35,326.58 W/m2 797.521 K
0.9c 106,195.696 W/m2 1050.131 K
0.99c 1,698,225.484 W/m2 2099.982 K
0.999c 18,973,260.691 W/m2 3839.303 K
Beyond
sublimation point [7]

Notes: Ice has an emissivity of 0.97, while Graphite has an emissivity of 0.7

The parameters vary with changing exposed area, area and emissivity, flux. What is clear here is that the interstellar medium flux can present a significant danger at high enough velocities as to sublimate (in the vacuum of space) ice, and at ever increasing velocity, even graphite.

Therefore, care must be taken to shield your interstellar spacecraft from the flux if it is moving at a velocity high enough to heat the spacecraft with disastrous consequences.

1. https://en.wikipedia.org/wiki/Interstellar_medium
Reference for ISM density
2. https://en.wikipedia.org/wiki/Interstellar_medium
Reference for ISM composition
3. H. Kruger et. al., "Sixteen Years of Ulysses Interstellar Dust Measurements in the Solar System. I. Mass Distribution and Gas-to-Dust Mass Ratio", Astrophysical Journal, October 20, 2015. https://ui.adsabs.harvard.edu/link_gateway/2015ApJ...812..139K/PUB_PDF
4. https://bis-space.com/shop/product/project-daedalus-demonstrating-the-engineering-feasibility-of-interstellar-travel/
Reference for the Daedalus report figure.
5. https://en.wikipedia.org/wiki/Stefan%E2%80%93Boltzmann_law
Stefan Boltzmann Law
6. https://en.wikipedia.org/wiki/Frost_line_%28astrophysics%29
Reference for ice sublimation
7. https://en.wikipedia.org/wiki/Carbon
Reference for graphite sublimation. I assume the point occurs at a lower temperature due to lower pressure.

## Derivation of the Relativistic Flux Equation

1. The kinetic energy of an amount of mass is given by ${\displaystyle (\gamma -1)mc^{2}}$. To get the power, the kinetic energy is differentiated against time and thus assuming constant velocity, obtain that with ${\displaystyle {\dot {m}}}$ (the mass flow rate); the power is given by ${\displaystyle (\gamma -1){\dot {m}}c^{2}}$.
2. The mass flow is given by the mass per volume encountered every second, doing this in the reference frame of the ship, the ISM density is length contracted to to ${\displaystyle \gamma \rho }$ and multiply by ${\displaystyle Av}$ where ${\displaystyle A}$ is area.
3. This yields ${\displaystyle P=\gamma \rho Av(\gamma -1)c^{2}}$, to obtain the flux per unit area divide by ${\displaystyle A}$ and thereby cancel the ${\displaystyle A}$ in the earlier expression.

Reference for the Derivation of the Relativistic Flux Equation

# Credit

To Tshhmon for writing the article

• To lwcamp for helping with erosion calculation
• To Kerr for the relativistic flux equation and derivation