thermal-energy-storage

Thermal energy storage

Subsystem Semi-native power
TRL Mars
Energy intensity
Required by
0
Requires
3

Stores energy as sensible heat in regolith, molten salt, or phase-change material. Three architectures: sensible-heat regolith / basalt (cheap, scalable, 30-40 % round-trip via Brayton), molten salt (Andasol heritage, 60Na/40K nitrate, commercial CSP plants since 2008), and phase-change (PCM, latent heat at fixed T — narrower temperature range but higher energy density). Mars-specific: bury thermal mass in regolith berm for free insulation; pair with solar concentrator or nuclear waste heat input; output via Brayton or organic Rankine.

Last reviewed: 2026-06-09

Governing equations

Sensible-heat storage energy. Basalt c_p ≈ 0.85 kJ/kg·K; ΔT 500 °C: 1 t basalt stores 425 MJ = 118 kWh thermal. At 35 % round-trip: 41 kWh electrical. [1]

Phase-change-material storage energy. Higher per kg than sensible heat but only over narrow T range. NaCl/KCl eutectic: 280 kJ/kg latent at ~ 660 °C. [1]

Full round-trip: electric → thermal heater (95 %) × storage retention (85 % over week) × Brayton conversion (40 %) = ~ 32 %. Comparable to fuel cell loop. [1]

Heat loss rate through insulation. Vacuum gap + MLI + regolith berm: < 1 %/day for industrial-scale buried tanks. Major operational variable for long-duration storage. [1]

Key constants & quantities

Symbol Value Units Conditions Description
c_p,basalt 0.85 kJ / kg · K Specific heat of basalt regolith. Comparable to Earth granite + concrete.[2]
E_specific,sensible-basalt 100 ±20 kWh/t kWh-thermal / t (ΔT 400 °C) Energy density of sensible-heat basalt storage at typical 400 °C swing. 1 t = 100 kWh-thermal = ~ 35 kWh-electrical out.[1]
E_specific,molten-salt 250 ±30 kWh/t kWh-thermal / t (Andasol nitrate salt, ΔT 290 °C) Solar-thermal molten salt storage (NaNO₃/KNO₃ Andasol mixture). Higher specific capacity than basalt; needs sealed tank to prevent crystallization.[3]
E_specific,PCM-salt 100 kWh-thermal / t (NaCl-KCl latent only) Phase-change material energy density at melt point. Narrower operating T but higher peak-T density.[1]
T_operating,Andasol 290–565 °C (Andasol molten salt range) Operational temperature range of Andasol-class molten-salt CSP. Higher T = better Brayton efficiency.[3]
T_operating,sensible-basalt 25–700 °C Wide operating range possible with basalt (no phase change limit). High-T limits set by container materials + heat exchanger.[1]
η_round-trip,thermal 30–40 ±5 % % (electrical-in to electrical-out) Full electric → heat → storage → Brayton → electric round-trip efficiency. Lower than battery; trade is mass + cost.[1]
Q_loss,buried 0.5 ±0.3 %/day %/day energy loss Heat loss for well-insulated buried thermal mass. Multi-month storage feasible at < 50 % loss.[1]

Operating envelope

ParameterRangeUnitsSource
Operating T range 25 – 800 °C [1]
Storage duration (practical) 1 – 180 days [3]
Heat-transfer fluid (sensible salt) 200 – 565 °C [3]
Round-trip electrical-to-electrical 25 – 40 % [1]
Brayton hot-side T (target) 600 – 1000 °C [1]

Mass balance

Basis: 36 MWh-thermal stored (matches H₂-storage scenario)

Inputs

Regolith / basalt thermal mass 360 t (sensible-heat at ΔT 400 °C) [2]
Heaters (resistive electric, Mars-import) 0.5 t [1]
Insulation (vacuum-MLI + regolith berm) 1.5 t [1]
Brayton turbine / engine 1.5 t (modular) [4]
  • Regolith / basalt thermal mass: Mars-mined; free material. Sized for the storm-survival scenario.
  • Heaters (resistive electric, Mars-import): Embedded electric resistance heaters for charging.
  • Insulation (vacuum-MLI + regolith berm): Multi-layer + buried installation; minimizes heat loss.
  • Brayton turbine / engine: Stirling or Brayton for thermal-to-electric conversion. Shared with nuclear-reactor architecture.

Outputs

Stored thermal energy 36,000 kWh-thermal [1]
Discharged electrical (at 35 % round-trip) 12,600 kWh-electrical recovered [1]
Available process heat (high-grade) 36,000 kWh-thermal direct use [1]
  • Discharged electrical (at 35 % round-trip): Lower yield than battery but mass-efficient at colony scale.
  • Available process heat (high-grade): Direct heat output usable for habitat warm-up, Sabatier preheat, sintering, etc.
TRL · Earth
9/ 9
TRL · Mars
5/ 9
Andasol-class molten-salt CSP: TRL 9 — commercial deployment since 2008 (Spain), Crescent Dunes (US 2015). Sensible-heat rock storage: TRL 7-8 — multiple commercial projects (Siemens Gamesa ETES, EnergyNest concrete). PCM thermal storage: TRL 6-7 — research-grade + small commercial deployment. Mars-base scale: TRL 5 — design transfer is straightforward; no flight unit.[3]
Energy budget
0 kWhe / capability (energy is stored heat; insulation losses are ongoing) [1]

Insulation losses ~ 0.5 %/day. For 36 MWh stored × 30 days: ~ 5 % cumulative loss. Mass-efficient regolith storage is the cheapest per-kWh option at large scale.

Variants & trade-offs

Sensible-heat regolith / basalt mass

[1]

Mars-mined regolith heated by embedded electric resistance heaters or solar concentrator. Buried thermal mass + MLI + regolith berm gives < 1 %/day loss. The cheapest mass-scalable storage for Mars colony.

Operating T
200–700 °C
Energy density
80–150 kWh-thermal / t
Insulation overhead
0.3–1 %/day loss
Stack lifetime
100000–500000 h (decades possible)
Materials: Mars regolith / basalt (mined + crushed + screened) · Resistance heater elements (Ni-Cr) · Vacuum-MLI insulation · Stainless heat exchanger to Brayton
  • Zero material cost (regolith is free)
  • No thermal cycling fatigue concerns at sensible-heat scale
  • Long-duration storage (months)
  • Compatible with sustainable Mars architecture
  • ~ 30-40 % round-trip efficiency
  • Slower discharge response than battery
  • Limited by Brayton/Stirling engine output capacity
  • High-T heat exchanger materials hard import

Molten salt (Andasol-class)

[3]

NaNO₃/KNO₃ nitrate salt mixture (60:40 wt) heated to 565 °C and stored in insulated tank. Used for solar-thermal CSP plants worldwide (Andasol 1-3 Spain, Crescent Dunes Nevada). Higher energy density than sensible basalt.

Operating T
290–565 °C
Energy density
200–300 kWh-thermal / t
Stack lifetime
100000–300000 h (30-50 years CSP operational)
Materials: NaNO₃ + KNO₃ molten salt (60:40) · Stainless 316L tank (high-T corrosion-resistant) · Pumps + valves for salt circulation · Stainless heat exchanger
  • 2-3× energy density of sensible basalt
  • Mature commercial deployment
  • Predictable thermal properties
  • Direct CSP coupling
  • NaNO₃ + KNO₃ are Mars-import-dependent (initial supply)
  • Salt freezes at 220 °C — never let cold
  • Corrosive to common metals at high T
  • Tank + plumbing complexity

Phase-change material (PCM, NaCl-KCl eutectic)

[1]

Storage at fixed-T phase change. NaCl/KCl eutectic melts at 657 °C with ~ 280 kJ/kg latent heat. Higher energy density at fixed operating T but narrower operating range.

Phase-change T
600–700 °C
Latent heat
200–350 kJ/kg
Stack lifetime
40000–150000 h
Materials: NaCl + KCl eutectic salt · Stainless containment + heat exchanger · Refractory insulation · Embedded heat-exchange tubes
  • Highest energy density per kg
  • Fixed T output convenient for downstream conversion
  • Higher T operation than nitrate salt
  • Narrower operating T range
  • Phase-change-cycle fatigue
  • Solid-liquid heat-transfer challenges
  • Lower TRL than sensible + molten-salt

When preferred: Narrow-temperature applications; specific high-T process heat coupling.

Failure modes

Mode Cause Detection Mitigation
Insulation degradation / increased losses[1] MLI compression damage, vacuum loss, regolith-berm erosion. Heat-loss rate climbs. Outer-wall thermal monitoring; energy-balance discrepancy. Redundant insulation layers; vacuum-gauge monitoring; periodic re-evacuation; conservative initial-loss budgets.
Heater element failure (sensible variant)[1] Resistive heater oxidation or burnout; Mars-cold-start thermal shock. Per-element resistance test; thermal-gradient monitoring. Redundant heater banks; conservative power ratings; field-replaceable element modules.
Molten salt freezing[3] Salt allowed below freezing point (NaNO₃ 220 °C). Re-melting requires significant energy input + can damage piping. Salt T monitoring; flow rate; emergency trace-heating status. Continuous trace-heating; redundant heaters; salt-circulation maintenance; never-cold operating protocol.
Tank corrosion (molten salt at high T)[3] NaNO₃/KNO₃ corrodes 316L stainless above 600 °C; pitting + grain-boundary attack. Periodic ultrasonic NDE; salt sampling for dissolved metals. Conservative max-T limits; high-Ni alloys (Inconel 625) for high-T sections; programmed inspection.
Heat exchanger fouling[1] Solid deposits from salt impurities or regolith dust accumulate on HX surface; thermal transfer degrades. HX ΔT trend; pressure drop across exchanger. Periodic chemical cleaning; redundant HX paths; conservative design margins.
Brayton turbine seal degradation[4] High-T turbine seal elastomer or metallic seal degrades over operational hours. Pressure decay; efficiency drift. Programmed seal replacement; redundant gas-turbine stages; field-replaceable seal cartridges.
Storage T excursion (overheating)[1] Heater control failure or insulation reduction allows T to exceed material limits. Multi-point T monitoring; auto-shutdown on T limit. Conservative material rating + 20 % margin; redundant T sensors; emergency cooling protocol.

Mars adjustments

Regolith as free mass at any scale[2]

Impact: Mars regolith is freely available; no mining cost beyond local excavation. Thermal storage at 50 t scale costs ~ 0$ in material — only the heater + insulation + Brayton cost.

Mitigation: Real benefit. Combined with nuclear or solar-concentrator heat input, regolith thermal mass is the cheapest energy reservoir.

Cold ambient improves insulation effectiveness[5]

Impact: Mars surface T -90 to +20 °C. ΔT from buried thermal storage (500 °C) to ambient is ~ 500 °C. Vacuum insulation + regolith berm gives < 1 %/day loss vs Earth equivalent at higher ambient.

Mitigation: Real benefit. Mars buried + insulated thermal storage outperforms Earth equivalent.

Co-located with nuclear or concentrating solar[4]

Impact: Nuclear reactor waste heat (1000 °C reactor core) or solar concentrator (500-1500 °C focus) directly charges thermal storage with minimal conversion loss.

Mitigation: Real benefit. Direct thermal coupling vs electric-resistance charging saves 5 % efficiency penalty.

Brayton engine + radiator co-location[4]

Impact: Brayton + radiator already deployed for nuclear-reactor architecture. Thermal storage shares this infrastructure for power output.

Mitigation: Real benefit. Modular Brayton sized to thermal storage; shared radiator capacity.

Long-duration storage feasibility[3]

Impact: Buried + insulated thermal storage can hold heat for months. Mars seasonal energy variability + storm-survival demands long-duration option that battery + H₂ cannot match economically.

Mitigation: Real benefit. Combines with other storage (battery for short; H₂ for medium; thermal for seasonal).

Alternatives & substitutes

Battery storage (short-duration)[6]

  • 92 % round-trip efficiency
  • Fast discharge response
  • Mature commercial supply chain
  • Mass-prohibitive at multi-week storage
  • Cold-soak performance constrained
  • High $/kWh stored

When preferred: Daily diurnal cycling; rapid-response load support; not multi-week storage.

Hydrogen storage (regenerative loop)[7]

  • Mass-efficient at large scale
  • Shared infrastructure with ECLSS + propellant
  • Cleaner regenerative cycle
  • 35-45 % round-trip efficiency (vs thermal 30-40 %, comparable)
  • Cryogenic complexity (LH₂)
  • Hydrogen embrittlement of metal

When preferred: Long-duration storage where mass-savings matter most.

Requires

References

  1. Bergman, T. L., Lavine, A. S., Incropera, F. P., & DeWitt, D. P. (2017). Fundamentals of Heat and Mass Transfer, 8th Edition. John Wiley & Sons. ISBN 978-1-119-32042-5. — Standard undergraduate / engineering reference for heat transfer: Stefan-Boltzmann radiation, conduction, convection.
  2. McLennan, S. M., Sephton, M. A., Beaty, D. W., Hecht, M., et al. (2014). Planning for Mars Returned Sample Science: Final Report of the MSR End-to-End International Science Analysis Group. NASA Mars Exploration Program Analysis Group (MEPAG). — Mars surface materials properties and ISRU planning; basis for water extraction system sizing.
  3. Solar Millennium AG (Andasol) / NREL CSP Database (2008). Andasol-1 Concentrating Solar Power Plant — Operational Data + Design Reference. NREL Concentrating Solar Power Projects Database + Solar Millennium AG operational reports. — Andasol 1-3 parabolic trough CSP (Spain, 2008+) — first commercial molten-salt storage + first 50 MW commercial parabolic trough. Reference for nitrate-salt thermal storage architecture.
  4. Mason, L., Gibson, M., Poston, D., Briggs, M., Sanzi, J., & Bell, J. (2018). A Small Fission Power System for NASA Exploration: KRUSTY Test Results. Nuclear and Emerging Technologies for Space (NETS) Conference, Las Vegas. NASA/TM-2018-219782. — KRUSTY full-power test 2018; Mars surface fission TRL 6 demonstration.
  5. Haberle, R. M., Clancy, R. T., Forget, F., Smith, M. D., & Zurek, R. W. (Eds.) (2017). The Atmosphere and Climate of Mars. Cambridge University Press. ISBN 978-1-107-01618-7. — Reference handbook for Mars atmospheric pressure, temperature, dust climatology.
  6. Whitacre, J. F. (2018). Battery Technologies for Grid-Scale Energy Storage. Annual Review of Chemical and Biomolecular Engineering, 9, 333-355. doi:10.1146/annurev-chembioeng-060817-084218 — Comprehensive review of Li-ion, LFP, NaS, redox flow chemistries; cycle life, safety, applications.
  7. U.S. Department of Energy (2020). Department of Energy Hydrogen Program Plan. U.S. Department of Energy, Office of Energy Efficiency and Renewable Energy. DOE/EE-2128. — Technical targets for water electrolyzer cost, durability, efficiency.