Carbon dioxide (two-phase pumped-loop coolant) CO2
CO2 · CAS 124-38-9
Carbon dioxide (CO2) is one carbon atom bonded to two oxygen atoms.
Evidence level
2 of 5
Lab-measured
- 0Predicted only. No one has made it, or no measurement exists.
- 1Calculated. Only calculated or predicted values from sources.
- 2Lab-measured. Measured properties with their conditions stated.
- 3Space-relevant tests. Measured in conditions relevant to space, such as vacuum or atomic oxygen.
- 4Ground-qualified. Qualified for an application on the ground.
- 5Flown or field-proven. Flight or field results exist.
Recipe, share of the weight
- C not statedCarbon
- O not statedOxygen
Best for
Pumped cooling loops on a space instrument where the coolant can be refilled on orbit, as NASA planned for the AMS-02 tracker
Weakest at
Narrow margins: the liquid exists only above the 5.185 bar triple-point pressure, and the AMS-02 pumps are the documented failure point
Risk at a glance
- People Low. Compressed gas; cold liquid can cause burns
- If it fails High. Coolant pump wear-out in the AMS-02 tracker loop
- Corrosion No data. No corrosion data recorded
Why it exists
Carbon dioxide is a coolant that stays liquid only under pressure. NASA's tracker cooling on the International Space Station circulated liquid carbon dioxide through a pumped loop, which is why its phase data matter for the design. The triple point and critical point set the pressure and temperature window in which the liquid can be held.
Where it's used
AMS-02 tracker on the International Space Station
NASA's spacewalk reports describe liquid carbon dioxide as the coolant of the AMS-02 silicon tracker. The crew replenished the instrument with it during the repair spacewalks.
Upgraded tracker thermal pump system
The upgraded system was installed on a later spacewalk and connected to the existing AMS cooling lines, with the new loop filled with carbon dioxide after leak checks.
Recipe
CO2
Carbon dioxide has one carbon atom bonded to two oxygen atoms. Industrially it is recovered as a byproduct of hydrogen production by steam reforming and of ammonia production, and from natural gas processing.
| Ingredient | Share of the weight | What it does |
|---|---|---|
| Carbon C | not stated | The central atom. Each carbon atom is bonded to two oxygen atoms in the molecule. |
| Oxygen O | not stated | The two outer atoms. Together with the carbon they make a molecule of molar mass 44.0095 amu. |
Weight shares are as printed in the sources.
What it can do
Strength
Carry heat away in a pumped liquid loop on a space instrument, as the AMS-02 tracker did.
Strength
Be refilled on orbit during spacewalks, which NASA planned for the AMS-02 tracker.
Strength
Stay liquid only above its triple-point pressure of 5.185 bar, at its triple-point temperature of 216.58 K and above.
How it compares
NIST's reference data for carbon dioxide give a critical point at 304.18 K and 73.80 bar, a triple point at 216.58 K and 5.185 bar, and an enthalpy of vaporization of 16.7 kJ/mol at 288 K. The table below lists three of these values. No other cooling fluid is compared, because the sources read for this profile give no same-basis values for one.
The same measurements for each material, so you can compare them. Each row names the key condition under the value; the full conditions and methods are in the numbered notes under Technical details.
| Measurement | CO2 |
|---|---|
| Thermal behavior and safety | |
| Enthalpy of vaporization | 16.7 kJ/mol8 |
| Enthalpy of vaporization | 16.4 kJ/mol9 |
| Enthalpy of vaporization | 16.5 kJ/mol10 |
| Lifetime and stability | |
| Critical volume | 0.0919 l/mol4 |
| Standard enthalpy of formation, gas | -393.5 kJ/mol14 |
| Standard entropy, gas at 1 bar | 213.8 J/mol*K15 |
| Physical and electrical | |
| Critical density | 10.6 mol/l3 |
| Temperature behavior | |
| Critical temperature | 304.2 K1 |
| Triple point temperature | 216.6 K5 |
| Other measurements | |
| Critical pressure | 73.8 bar2 |
| Triple point pressure | 5.185 bar6 |
| Molecular weight | 44.01 amu7 |
| Enthalpy of sublimation | 26.1 kJ/mol11 |
| Enthalpy of sublimation | 26.3 kJ/mol12 |
| Enthalpy of sublimation | 25.2 kJ/mol13 |
Why choose it, and why not
Good for
- Pumped cooling loops on space instruments, where NASA used liquid carbon dioxide on the AMS-02 tracker.
- Reference thermodynamic data: NIST gives the triple point and critical point with stated uncertainties.
Watch out for
- Pumps: the AMS-02 record shows coolant pumps that wore out well past their design life.
- Pressure: the liquid exists only above the triple-point pressure of 5.185 bar.
- Heat: the gas is under pressure and may explode when heated (PubChem H280).
Carbon dioxide has well-measured phase data for a pumped loop. On the AMS-02 record, the pumps failed before the fluid did, and the repair was a refill and replacement of the loop.
Technical details
For scientists and researchers. Everything above comes from the record below: every number with its method, its conditions and its source.
Notes
The method, full conditions and any caveat for the numbered rows above.
| # | Measurement | Method | Conditions | Caveat |
|---|---|---|---|---|
| 1 | Critical temperature | Critical temperature as tabulated by NIST; NIST assigns an uncertainty of 0.04 K (TRC). Other rows in the same table give 304.1 K to 304.35 K. | phase critical point, liquid and vapourreference row Suehiro, Nakajima, et al., 1996 | — |
| 2 | Critical pressure | Critical pressure as tabulated by NIST; NIST assigns an uncertainty of 0.15 bar (TRC). | phase critical pointreference row Suehiro, Nakajima, et al., 1996 | — |
| 3 | Critical density | Critical density as tabulated by NIST; NIST assigns an uncertainty of 0.05 mol/l (TRC). Angus et al. 1976 gives 10.590 mol/l. | phase critical pointreference row Suehiro, Nakajima, et al., 1996 | — |
| 4 | Critical volume | Critical volume as tabulated by NIST (uncertainty 0.001 l/mol, TRC). | phase critical point | — |
| 5 | Triple point temperature | Triple-point temperature as tabulated by NIST; NIST assigns an uncertainty of 0.008 K (TRC) and recommends it as a thermometry fixed point. Angus et al. 1976 gives the same 216.58 K. | basis solid, liquid and vapour in equilibriumreference row Marsh, 1987 | — |
| 6 | Triple point pressure | Triple-point pressure as tabulated by NIST; NIST assigns an uncertainty of 0.005 bar (TRC). | basis solid, liquid and vapour in equilibriumreference row Angus, Armstrong, et al., 1976 | — |
| 7 | Molecular weight | Molecular weight as printed on the NIST WebBook compound page (IUPAC Gold Book link). | basis molecular weight of CO2 as printed by NIST | — |
| 8 | Enthalpy of vaporization | Enthalpy of vaporization as tabulated by NIST from Stephenson and Malanowski, 1987, based on data from 273 K to 304 K. | temperature 288 Kbasis liquid to vapour transition | — |
| 9 | Enthalpy of vaporization | Enthalpy of vaporization as tabulated by NIST from Stephenson and Malanowski, 1987, based on data from 216 K to 273 K. | temperature 258 Kbasis liquid to vapour transition | — |
| 10 | Enthalpy of vaporization | Enthalpy of vaporization as tabulated by NIST from Boublik and Aim, 1972, based on data from 267 K to 303 K. | temperature 282 Kbasis liquid to vapour transition | — |
| 11 | Enthalpy of sublimation | Enthalpy of sublimation as tabulated by NIST from Stephenson and Malanowski, 1987, based on data from 198 K to 216 K. | temperature 207 Kbasis solid to vapour transition | — |
| 12 | Enthalpy of sublimation | Enthalpy of sublimation as tabulated by NIST from Stull, 1947, based on data from 139 K to 195 K. | temperature 167 Kbasis solid to vapour transition | — |
| 13 | Enthalpy of sublimation | Enthalpy of sublimation as tabulated by NIST from Giauque and Egan, 1937, based on data from 154 K to 196 K. | temperature 195 Kbasis solid to vapour transition | — |
| 14 | Standard enthalpy of formation, gas | CODATA review value as printed by NIST (Cox, Wagman, et al., 1984). Chase, 1998 gives -393.52 kJ/mol. | state gas at standard conditionsuncertainty plus or minus 0.13 kJ/mol as printed | — |
| 15 | Standard entropy, gas at 1 bar | CODATA review value as printed by NIST (Cox, Wagman, et al., 1984). Chase, 1998 gives 213.79 J/mol*K. | state gas at 1 bar standard pressureuncertainty plus or minus 0.010 J/mol*K as printed | — |
Risks and side effects
Hazards to people, what happens when a cell overheats, and how the material is handled and stored.
For people
PubChem lists the compressed-gas hazard (H280) and the cold-burn hazard (H281) for carbon dioxide.
- Pressure
- The gas is under pressure and may explode if heated. Keep containers away from heat.
- Cold
- Refrigerated or liquid carbon dioxide can cause cryogenic burns or injury.
If a pumped loop fails
The AMS-02 record shows how coolant-loop trouble appeared on orbit.
- Pumps
- Most of the coolant pumps had stopped, and the last one ran only intermittently under good sunlight conditions.
- Repair
- The repair installed a new loop on spacewalks, followed by leak checks and a refill with carbon dioxide.
Handling and storage
- Storage
- Keep containers closed and away from heat, since the gas may explode when heated.
- Venting
- The crew vented the carbon dioxide left in the old pump before cutting its lines.
Test details
The original wording and numbers from the sources, for readers who want them.
Failure risks
| Failure | Trigger and consequence |
|---|---|
| Coolant pump wear-out in the AMS-02 tracker loophigh severity | Pumps run far beyond their original design life on orbitNASA reported that most of the coolant pumps had stopped, and the last one ran only intermittently under good sunlight conditions, so the cooling system was close to stopping altogether. |
| Leak in a cooling line after the loop is rebuiltmoderate severity | Fluid-line work during spacewalksLeak checks are a required step before the loop is trusted. The 2020 spacewalk completed leak checks and opened a valve to begin pressurizing the system. |
Handling and storage
- Keep containers closed and away from heat. The gas is under pressure and may explode if heated (PubChem H280).
- Protect skin and eyes from refrigerated or liquid carbon dioxide, which can cause cryogenic burns (PubChem H281).
- Before cutting lines on orbit, the crew vented the carbon dioxide that remained in the old cooling pump.
- After leak checks, ground teams filled the new AMS thermal control system with carbon dioxide and then powered the pumps.
Supply and geography
How common the raw materials are and where they come from.
Carbon dioxide (industrial supply)
- Recycling
- Not stated in the source used.
Documents
Datasheets, safety data sheets, papers and standards you can open.
| Document | Type | Year |
|---|---|---|
| NIST WebBook: carbon dioxide phase change data (CAS 124-38-9) | database | 2026 |
| NIST WebBook: carbon dioxide gas phase thermochemistry | database | 2026 |
| PubChem: Carbon dioxide (CID 280), GHS classification | database | 2026 |
| NASA Space Station blog: second cosmic repair spacewalk | report | 2019 |
Full record
The complete spore, as stored. Free to reuse under CC-BY-4.0. Images keep the licence shown with each one.
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spore: profile
id: carbon-dioxide-two-phase-coolant
spore_version: 0.2
family: carbon-dioxide
name: Carbon dioxide (two-phase pumped-loop coolant)
abbreviation: CO2
role: coolant
category: thermal-protection
type: multi-layer-insulation
summary: |
Carbon dioxide (CO2) is one carbon atom bonded to two oxygen atoms. NIST's reference data put its triple point at 216.58 K and 5.185 bar, and its critical point at 304.18 K and 73.80 bar, so liquid CO2 exists only above the triple-point pressure. NASA used liquid carbon dioxide as the coolant in the pumped loop that cools the silicon tracker of the Alpha Magnetic Spectrometer (AMS-02) on the International Space Station.
best_for: Pumped cooling loops on a space instrument where the coolant can be refilled on orbit, as NASA planned for the AMS-02 tracker
weakest_at: 'Narrow margins: the liquid exists only above the 5.185 bar triple-point pressure, and the AMS-02 pumps are the documented failure point'
identity:
formula: CO2
cas: 124-38-9
source: nist-phase
where: 'NIST WebBook compound page header: CAS Registry Number 124-38-9 and molecular weight 44.0095'
tags:
applications:
- thermal-control
properties:
- benchmark: critical_temperature
label: Critical temperature
value: 304.18
unit: K
scope: material
conditions:
phase: critical point, liquid and vapour
reference_row: Suehiro, Nakajima, et al., 1996
method: Critical temperature as tabulated by NIST; NIST assigns an uncertainty of 0.04 K (TRC). Other rows in the same table give 304.1 K to 304.35 K.
status: ground
source: nist-phase
where: Phase change data table, Tc row (Suehiro, Nakajima, et al., 1996)
- benchmark: critical_pressure
label: Critical pressure
value: 73.8
unit: bar
scope: material
conditions:
phase: critical point
reference_row: Suehiro, Nakajima, et al., 1996
method: Critical pressure as tabulated by NIST; NIST assigns an uncertainty of 0.15 bar (TRC).
status: ground
source: nist-phase
where: Phase change data table, Pc row (Suehiro, Nakajima, et al., 1996)
- benchmark: critical_density
label: Critical density
value: 10.6
unit: mol/l
scope: material
conditions:
phase: critical point
reference_row: Suehiro, Nakajima, et al., 1996
method: Critical density as tabulated by NIST; NIST assigns an uncertainty of 0.05 mol/l (TRC). Angus et al. 1976 gives 10.590 mol/l.
status: ground
source: nist-phase
where: Phase change data table, rho c row (Suehiro, Nakajima, et al., 1996)
- benchmark: critical_volume
label: Critical volume
value: 0.0919
unit: l/mol
scope: material
conditions:
phase: critical point
method: Critical volume as tabulated by NIST (uncertainty 0.001 l/mol, TRC).
status: ground
source: nist-phase
where: Phase change data table, Vc row (Li and Kiran, 1988)
- benchmark: triple_point_temperature
label: Triple point temperature
value: 216.58
unit: K
scope: material
conditions:
basis: solid, liquid and vapour in equilibrium
reference_row: Marsh, 1987
method: Triple-point temperature as tabulated by NIST; NIST assigns an uncertainty of 0.008 K (TRC) and recommends it as a thermometry fixed point. Angus et al. 1976 gives the same 216.58 K.
status: ground
source: nist-phase
where: Phase change data table, Ttriple row (Marsh, 1987)
- benchmark: triple_point_pressure
label: Triple point pressure
value: 5.185
unit: bar
scope: material
conditions:
basis: solid, liquid and vapour in equilibrium
reference_row: Angus, Armstrong, et al., 1976
method: Triple-point pressure as tabulated by NIST; NIST assigns an uncertainty of 0.005 bar (TRC).
status: ground
source: nist-phase
where: Phase change data table, Ptriple row (Angus, Armstrong, et al., 1976)
- benchmark: molar_mass
label: Molecular weight
value: 44.0095
unit: amu
scope: material
conditions:
basis: molecular weight of CO2 as printed by NIST
method: Molecular weight as printed on the NIST WebBook compound page (IUPAC Gold Book link).
status: ground
source: nist-phase
where: Molecular weight line on the NIST WebBook page header
- benchmark: enthalpy_of_vaporization
label: Enthalpy of vaporization
value: 16.7
unit: kJ/mol
scope: material
conditions:
temperature: 288 K
basis: liquid to vapour transition
method: Enthalpy of vaporization as tabulated by NIST from Stephenson and Malanowski, 1987, based on data from 273 K to 304 K.
status: ground
source: nist-phase
where: Enthalpy of vaporization table, first row (Stephenson and Malanowski, 1987)
- benchmark: enthalpy_of_vaporization
label: Enthalpy of vaporization
value: 16.4
unit: kJ/mol
scope: material
conditions:
temperature: 258 K
basis: liquid to vapour transition
method: Enthalpy of vaporization as tabulated by NIST from Stephenson and Malanowski, 1987, based on data from 216 K to 273 K.
status: ground
source: nist-phase
where: Enthalpy of vaporization table, second row (Stephenson and Malanowski, 1987)
- benchmark: enthalpy_of_vaporization
label: Enthalpy of vaporization
value: 16.5
unit: kJ/mol
scope: material
conditions:
temperature: 282 K
basis: liquid to vapour transition
method: Enthalpy of vaporization as tabulated by NIST from Boublik and Aim, 1972, based on data from 267 K to 303 K.
status: ground
source: nist-phase
where: Enthalpy of vaporization table, third row (Boublik and Aim, 1972)
- benchmark: enthalpy_of_sublimation
label: Enthalpy of sublimation
value: 26.1
unit: kJ/mol
scope: material
conditions:
temperature: 207 K
basis: solid to vapour transition
method: Enthalpy of sublimation as tabulated by NIST from Stephenson and Malanowski, 1987, based on data from 198 K to 216 K.
status: ground
source: nist-phase
where: Enthalpy of sublimation table, first row (Stephenson and Malanowski, 1987)
- benchmark: enthalpy_of_sublimation
label: Enthalpy of sublimation
value: 26.3
unit: kJ/mol
scope: material
conditions:
temperature: 167 K
basis: solid to vapour transition
method: Enthalpy of sublimation as tabulated by NIST from Stull, 1947, based on data from 139 K to 195 K.
status: ground
source: nist-phase
where: Enthalpy of sublimation table (Stull, 1947)
- benchmark: enthalpy_of_sublimation
label: Enthalpy of sublimation
value: 25.2
unit: kJ/mol
scope: material
conditions:
temperature: 195 K
basis: solid to vapour transition
method: Enthalpy of sublimation as tabulated by NIST from Giauque and Egan, 1937, based on data from 154 K to 196 K.
status: ground
source: nist-phase
where: Enthalpy of sublimation table (Giauque and Egan, 1937)
- benchmark: enthalpy_of_formation_gas
label: Standard enthalpy of formation, gas
value: -393.51
unit: kJ/mol
scope: material
conditions:
state: gas at standard conditions
uncertainty: plus or minus 0.13 kJ/mol as printed
method: CODATA review value as printed by NIST (Cox, Wagman, et al., 1984). Chase, 1998 gives -393.52 kJ/mol.
status: ground
source: nist-thermo
where: Gas phase thermochemistry data, delta-f H gas row (Cox, Wagman, et al., 1984)
- benchmark: entropy_gas_standard
label: Standard entropy, gas at 1 bar
value: 213.785
unit: J/mol*K
scope: material
conditions:
state: gas at 1 bar standard pressure
uncertainty: plus or minus 0.010 J/mol*K as printed
method: CODATA review value as printed by NIST (Cox, Wagman, et al., 1984). Chase, 1998 gives 213.79 J/mol*K.
status: ground
source: nist-thermo
where: Gas phase thermochemistry data, S gas row (Cox, Wagman, et al., 1984)
risks:
hazards:
- text: 'PubChem''s GHS entry for carbon dioxide gives H280: contains gas under pressure; may explode if heated. The signal word is Warning, and the pictogram is the compressed-gas symbol.'
ghs:
- H280
source: pubchem-ghs
where: GHS Classification section, Hazard Statements (ECHA C&L entries, CID 280)
- text: 'PubChem also lists H281 for carbon dioxide: contains refrigerated gas; may cause cryogenic burns or injury. This applies to the cold liquid or refrigerated form.'
ghs:
- H281
source: pubchem-ghs
where: GHS Classification section, Hazard Statements (ECHA C&L entries, CID 280)
failure_risks:
- mode: Coolant pump wear-out in the AMS-02 tracker loop
trigger: Pumps run far beyond their original design life on orbit
consequence: NASA reported that most of the coolant pumps had stopped, and the last one ran only intermittently under good sunlight conditions, so the cooling system was close to stopping altogether.
severity: high
source: spaceflightnow-2019
where: Article paragraphs on the four coolant pumps and the expected loss of cooling
- mode: Leak in a cooling line after the loop is rebuilt
trigger: Fluid-line work during spacewalks
consequence: Leak checks are a required step before the loop is trusted. The 2020 spacewalk completed leak checks and opened a valve to begin pressurizing the system.
severity: moderate
source: nasa-2020-01-25
where: Spacewalk summary paragraph, leak checks and pressurization
handling:
- text: Keep containers closed and away from heat. The gas is under pressure and may explode if heated (PubChem H280).
source: pubchem-ghs
where: GHS Classification section, H280 hazard statement
- text: Protect skin and eyes from refrigerated or liquid carbon dioxide, which can cause cryogenic burns (PubChem H281).
source: pubchem-ghs
where: GHS Classification section, H281 hazard statement
- text: Before cutting lines on orbit, the crew vented the carbon dioxide that remained in the old cooling pump.
source: nasa-2019-11-22
where: Summary paragraph on tube cutting and venting
- text: After leak checks, ground teams filled the new AMS thermal control system with carbon dioxide and then powered the pumps.
source: nasa-2020-01-25
where: Spacewalk summary paragraph, fill and pump power-on
uses:
- application: thermal-control
device: AMS-02 silicon tracker coolant loop on the International Space Station (flight, original pumped system)
example: NASA's spacewalk reporting describes the AMS tracker coolant as liquid carbon dioxide, which the astronauts would replenish during the repair spacewalks.
source: spaceflightnow-2019
where: Article paragraph on carbon dioxide coolant and replenishment
- application: thermal-control
device: Upgraded tracker thermal pump system on the International Space Station (flight, installed during spacewalks)
example: The crew installed the upgraded tracker thermal pump system and connected all the AMS cooling lines to the new system by swaging, a metalworking connection.
source: nasa-2019-12-02
where: Spacewalk summary paragraph on the upgraded tracker thermal pump system
supply:
- subject: Carbon dioxide (industrial supply)
producers: []
critical_lists: []
recycling: Not stated in the source used.
substitutes: []
source: wiki-co2
where: 'Industrial and geological sources section: byproduct of hydrogen production by steam reforming and of ammonia production, and from natural gas processing. No country production shares are given.'
story:
recipe:
line: Carbon dioxide has one carbon atom bonded to two oxygen atoms. Industrially it is recovered as a byproduct of hydrogen production by steam reforming and of ammonia production, and from natural gas processing.
parts:
- name: Carbon
symbol: C
role: The central atom. Each carbon atom is bonded to two oxygen atoms in the molecule.
- name: Oxygen
symbol: O
role: The two outer atoms. Together with the carbon they make a molecule of molar mass 44.0095 amu.
risk_groups:
- title: For people
level: 1
verdict: Compressed gas; cold liquid can cause burns
lead: PubChem lists the compressed-gas hazard (H280) and the cold-burn hazard (H281) for carbon dioxide.
points:
- label: Pressure
line: The gas is under pressure and may explode if heated. Keep containers away from heat.
- label: Cold
line: Refrigerated or liquid carbon dioxide can cause cryogenic burns or injury.
- title: If a pumped loop fails
lead: The AMS-02 record shows how coolant-loop trouble appeared on orbit.
points:
- label: Pumps
line: Most of the coolant pumps had stopped, and the last one ran only intermittently under good sunlight conditions.
- label: Repair
line: The repair installed a new loop on spacewalks, followed by leak checks and a refill with carbon dioxide.
- title: Handling and storage
points:
- label: Storage
line: Keep containers closed and away from heat, since the gas may explode when heated.
- label: Venting
line: The crew vented the carbon dioxide left in the old pump before cutting its lines.
why: Carbon dioxide is a coolant that stays liquid only under pressure. NASA's tracker cooling on the International Space Station circulated liquid carbon dioxide through a pumped loop, which is why its phase data matter for the design. The triple point and critical point set the pressure and temperature window in which the liquid can be held.
uses:
- where: AMS-02 tracker on the International Space Station
line: NASA's spacewalk reports describe liquid carbon dioxide as the coolant of the AMS-02 silicon tracker. The crew replenished the instrument with it during the repair spacewalks.
- where: Upgraded tracker thermal pump system
line: The upgraded system was installed on a later spacewalk and connected to the existing AMS cooling lines, with the new loop filled with carbon dioxide after leak checks.
can_do:
- label: Strength
line: Carry heat away in a pumped liquid loop on a space instrument, as the AMS-02 tracker did.
- label: Strength
line: Be refilled on orbit during spacewalks, which NASA planned for the AMS-02 tracker.
- label: Strength
line: Stay liquid only above its triple-point pressure of 5.185 bar, at its triple-point temperature of 216.58 K and above.
compare: NIST's reference data for carbon dioxide give a critical point at 304.18 K and 73.80 bar, a triple point at 216.58 K and 5.185 bar, and an enthalpy of vaporization of 16.7 kJ/mol at 288 K. The table below lists three of these values. No other cooling fluid is compared, because the sources read for this profile give no same-basis values for one.
compare_rows:
- label: Critical temperature
benchmark: critical_temperature
- label: Triple point temperature
benchmark: triple_point_temperature
- label: Enthalpy of vaporization
benchmark: enthalpy_of_vaporization
handling:
- Keep the container closed and away from heat. The gas is under pressure and may explode if heated.
- Protect skin and eyes from refrigerated or liquid carbon dioxide, which can cause cryogenic burns.
- On orbit, refill the loop only after leak checks, as the NASA crew and ground teams did.
good_for:
- Pumped cooling loops on space instruments, where NASA used liquid carbon dioxide on the AMS-02 tracker.
- 'Reference thermodynamic data: NIST gives the triple point and critical point with stated uncertainties.'
watch_out:
- 'Pumps: the AMS-02 record shows coolant pumps that wore out well past their design life.'
- 'Pressure: the liquid exists only above the triple-point pressure of 5.185 bar.'
- 'Heat: the gas is under pressure and may explode when heated (PubChem H280).'
verdict: Carbon dioxide has well-measured phase data for a pumped loop. On the AMS-02 record, the pumps failed before the fluid did, and the repair was a refill and replacement of the loop.
sources:
nist-phase:
title: 'NIST Chemistry WebBook: carbon dioxide, phase change data (NIST SRD 69)'
id: CAS 124-38-9
url: https://webbook.nist.gov/cgi/cbook.cgi?Mask=4&ID=C124389
year: 2026
kind: database
license: NIST Standard Reference Data (cited, not reproduced)
nist-thermo:
title: 'NIST Chemistry WebBook: carbon dioxide, gas phase thermochemistry data (NIST SRD 69)'
id: CAS 124-38-9
url: https://webbook.nist.gov/cgi/cbook.cgi?ID=C124389&Mask=1
year: 2026
kind: database
license: NIST Standard Reference Data (cited, not reproduced)
pubchem-ghs:
title: PubChem compound record, Carbon dioxide (CID 280), GHS classification
id: CID 280
url: https://pubchem.ncbi.nlm.nih.gov/rest/pug_view/data/compound/280/JSON?heading=GHS+Classification
year: 2026
kind: database
license: public domain (NCBI)
nasa-2019-11-22:
title: Astronauts Complete Intricate Tasks During Second Cosmic Repair Spacewalk (NASA blog)
id: NASA Space Station blog, 22 November 2019
url: https://www.nasa.gov/blogs/spacestation/2019/11/22/astronauts-complete-intricate-tasks-during-second-cosmic-repair-spacewalk/
year: 2019
kind: web
license: public domain (NASA)
nasa-2019-12-02:
title: Astronauts Wrap Up Third Spacewalk for Cosmic Particle Detector Repairs (NASA blog)
id: NASA Space Station blog, 2 December 2019
url: https://www.nasa.gov/blogs/spacestation/2019/12/02/astronauts-wrap-up-third-spacewalk-for-cosmic-particle-detector-repairs/
year: 2019
kind: web
license: public domain (NASA)
nasa-2020-01-25:
title: Astronauts Wrap Up Spacewalk Repair Job on Cosmic Ray Detector (NASA blog)
id: NASA Space Station blog, 25 January 2020
url: https://www.nasa.gov/blogs/spacestation/2020/01/25/astronauts-wrap-up-spacewalk-repair-job-on-cosmic-ray-detector/
year: 2020
kind: web
license: public domain (NASA)
spaceflightnow-2019:
title: Repair equipment for particle physics experiment aboard next station cargo launch (Spaceflight Now)
id: Spaceflight Now, 1 November 2019
url: https://spaceflightnow.com/2019/11/01/repair-equipment-for-particle-physics-experiment-aboard-next-station-cargo-launch/
year: 2019
kind: web
license: news article, linked not reproduced
wiki-co2:
title: Carbon dioxide (Wikipedia), sections on industrial sources and refrigerant use
id: Wikipedia article, Carbon dioxide
url: https://en.wikipedia.org/wiki/Carbon_dioxide
year: 2026
kind: web
license: CC BY-SA 4.0 (linked, not reproduced)
documents:
- title: 'NIST WebBook: carbon dioxide phase change data (CAS 124-38-9)'
type: database
url: https://webbook.nist.gov/cgi/cbook.cgi?Mask=4&ID=C124389
year: 2026
- title: 'NIST WebBook: carbon dioxide gas phase thermochemistry'
type: database
url: https://webbook.nist.gov/cgi/cbook.cgi?ID=C124389&Mask=1
year: 2026
- title: 'PubChem: Carbon dioxide (CID 280), GHS classification'
type: database
url: https://pubchem.ncbi.nlm.nih.gov/compound/280
year: 2026
- title: 'NASA Space Station blog: second cosmic repair spacewalk'
type: report
url: https://www.nasa.gov/blogs/spacestation/2019/11/22/astronauts-complete-intricate-tasks-during-second-cosmic-repair-spacewalk/
year: 2019
gaps:
- No flight or space-environment test data for the fluid's own properties in any source fetched; the only space source is the AMS-02 operations record.
- Corrosion or material-compatibility data for carbon dioxide in cooling-line materials were not found in any source opened, so the corrosion section is left out.
- 'Two-phase operation: the planner''s name says two-phase, but none of the fetched sources calls the AMS-02 loop two-phase. They describe liquid carbon dioxide in a pumped loop. The name is kept as the planner gave it and is not verified.'
- No country production shares for carbon dioxide were found; the supply section is qualitative and cites the Wikipedia sources section.
- No USGS or EU critical-minerals entry was checked for carbon dioxide, so critical_lists is left empty.
- 'Property names are not in spores/property-canon.yaml and were not invented to match it: critical_temperature, critical_pressure, critical_density, critical_volume, triple_point_temperature, triple_point_pressure, molar_mass, enthalpy_of_vaporization, enthalpy_of_sublimation, enthalpy_of_formation_gas and entropy_gas_standard.'
- NIST gives several critical-point rows from different references (for example 304.1 K to 304.35 K). Only one row is recorded per quantity; the others are named in the method text.
- No safety data sheet for carbon dioxide was opened. PubChem's ECHA-derived GHS entry was read through its REST view, because the HTML page showed a bot check.
- NIST fit coefficients (Antoine and Shomate) were not recorded as properties.
- Spaceflight Now blocks automated access, so its statements were read through WebFetch in this run and are not checked by the value script.
- Carbon dioxide's loop temperature and pressure operating ranges were not found in any source opened.
- No thermal-protection type fits a coolant. The type is set to multi-layer-insulation, the same as the methanol heat-pipe fluid profile, because the schema requires a type; a coolant type would need a taxonomy change.
license: CC-BY-4.0
updated: '2026-11-01'
review:
status: draft
method: assistant
checked_values: 15
unreachable: 0
caveats: 1
note: Written by an AI assistant on 2026-11-01. NIST and PubChem values were checked against the raw pages in this run.
References
Every number above carries a reference number. Click one to see the source and where in it the value comes from.
| # | Source | Type | Year | Used for |
|---|---|---|---|---|
| NIST Chemistry WebBook: carbon dioxide, phase change data (NIST SRD 69) | database | 2026 | 14 values | |
| NIST Chemistry WebBook: carbon dioxide, gas phase thermochemistry data (NIST SRD 69) | database | 2026 | 2 values | |
| PubChem compound record, Carbon dioxide (CID 280), GHS classification | database | 2026 | 4 values | |
| Astronauts Complete Intricate Tasks During Second Cosmic Repair Spacewalk (NASA blog) | web | 2019 | 1 value | |
| Astronauts Wrap Up Third Spacewalk for Cosmic Particle Detector Repairs (NASA blog) | web | 2019 | 1 value | |
| Astronauts Wrap Up Spacewalk Repair Job on Cosmic Ray Detector (NASA blog) | web | 2020 | 2 values | |
| Repair equipment for particle physics experiment aboard next station cargo launch (Spaceflight Now) | web | 2019 | 2 values | |
| Carbon dioxide (Wikipedia), sections on industrial sources and refrigerant use | web | 2026 | 1 value |
Updated