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Where would Mars crews get power, even during long dust storms?

Research question: Where would a crew get power on Mars, and how do they keep solar panels or a reactor working through long dust storms?

The records show that the proposed Mars colony power source is a nuclear fission surface power system with a total capacity of 1 MWel 17, and the planned system uses three 333 kWe reactors to supply 1 MWe for 15 years, with redundancy as backup if one unit fails 22. Dust storms reduce solar power by blocking sunlight and by settling on panels 1, and the InSight lander responded by entering safe mode 3 and limiting science instrument operating time 4. Natural cleaning can help solar arrays, since dust devils can remove dust 7 and a dust-clearing season from November to January uses winds to clean panels 6, but none had cleared dust from InSight by the time of its report 2. The facts do not describe how a reactor's output would be affected by dust storms, because the dust-related evidence concerns solar arrays 1. The newest fact dates to 2026 11, though it concerns a heat and power system's mass rather than dust storm operations.

Checked 2026-10-21. Only documented and supported facts are used.
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Sources

[1] supported
Dust storms reduce solar power on Mars by both blocking sunlight through the atmosphere and accumulating physically on the panels.
"Dust storms can affect solar panels in two ways: Dust reduces sunlight filtering through the atmosphere, and it can also accumulate on the panels."
NASA’s InSight Sees Power Levels Stabilize After Dust Storm - NASA
[2] documented
While whirlwinds have cleared dust from solar panels on previous missions like Spirit and Opportunity, none had cleared dust from the InSight lander by the time of the report.
"The whirlwinds and gusts of dust storms have helped to clear solar panels over time, as with the Spirit and Opportunity Mars rover missions. While InSight’s weather sensors have detected many passing whirlwinds, none have cleared any dust."
NASA’s InSight Sees Power Levels Stabilize After Dust Storm - NASA
[3] documented
InSight entered safe mode to conserve energy during a regional dust storm, a state where it suspends all non-essential functions to prevent battery drain.
"NASA’s InSight lander is stable and sending health data from Mars to Earth after going into safe mode Friday, Jan. 7, following a large, regional dust storm that reduced the sunlight reaching its solar panels. In safe mode, a spacecraft suspends all but its essential functions."
NASA’s InSight Sees Power Levels Stabilize After Dust Storm - NASA
[4] documented
The InSight team conserves energy by limiting the operating time of science instruments to extend the lander's life as dust accumulation reduces its power budget.
"The team anticipates that continued dust accumulation will progressively diminish the spacecraft’s overall power budget in the months ahead and has been carefully conserving energy by turning on science instruments for limited periods of time."
NASA’s InSight Sees Power Levels Stabilize After Dust Storm - NASA
[5] documented
Opportunity rover is solar-powered and relies on sunlight to recharge its batteries, which can be blocked by dust.
"It's possible that a layer of dust deposited on the rover's solar panels by the recent global dust storm is blocking sunlight that could recharge its batteries."
Update on Opportunity Rover Recovery Efforts
[6] supported
A specific seasonal period on Mars, known as 'dust-clearing season' from November to January, helps clean dust off solar panels via winds.
"A windy period on Mars -- known to Opportunity's team as "dust-clearing season" -- occurs in the November-to-January time frame and has helped clean the rover's panels in the past."
Update on Opportunity Rover Recovery Efforts
[7] supported
Dust devils on Mars can act as 'cleaning events' that remove dust from solar arrays, causing battery power levels to increase unexpectedly during the night.
"These cleaning dust devils have even been imaged by both rovers on the surface and spacecraft in orbit... battery power levels aboard both Spirit and Opportunity increased by several percent during a single Martian night, when the logical expectation was that they would continue to decrease."
Update on Opportunity Rover Recovery Efforts
[8] documented
The rovers were originally designed for only 90-day missions, with the expectation that extreme winters and dust storms would cut their missions short.
"Both Opportunity and its twin, Spirit, were designed to last only 90 days on the Martian surface, with the expectation that the planet's extreme winters and dust storms could cut their mission short."
Update on Opportunity Rover Recovery Efforts
[9] supported
Opportunity rover has operated for nearly 15 years, far exceeding its expected lifespan, despite challenges like dust storms and mechanical failures.
"The rover has lasted nearly 15 years: It last communicated on June 10 before being forced into hibernation by the growing dust storm."
Update on Opportunity Rover Recovery Efforts
[10] documented
Short circuit current in solar cells typically rebounds after they are cleaned of Mars dust.
"Short circuit current typically rebounds after solar cell is cleaned of Mars dust."
A study of photovoltaic degradation modes due to dust interaction on Mars - ScienceDirect
[11] documented
The combined heat and power system achieves a total mass of approximately 34.5 metric tons.
"The TOPSIS compromise solution achieves a discharging–heating exergy efficiency of 71.31%, a round-trip performance coefficient of 2.3716, and a total mass of 34,526.18 kg."
Performance assessment and surrogate-assisted multi-objective optimization of an SMSR-driven S-CO2 recompression Brayton–PTES combined heat and power system for Mars surface applications (2026)
[12] documented
During the 1971 global dust storm, suspended dust was raised to altitudes above 50 km, which would significantly obscure solar power sources.
"The greatest dust storm observed on Mars began in 1971 before the arrival of Mariner 9, obscured nearly all of the planet’s surface for several months, and raised dust up above 50 km in altitude."
NASA Technical Reports Server (NTRS) 19910017768: Dust in the Mars atmosphere (1991)
[13] documented
Dust storms on Mars are driven by a fluid-dynamic feedback loop where suspended dust absorbs solar radiation, heats the atmosphere, and alters pressure gradients to modify winds.
"General circulation modeling indicates that the rapid development and the variability of these storms are due to a Native-dynamic feedback in which suspended dust absorbs solar radiation, heats the atmosphere and thereby alters pressure gradients. This, in turn, modifies the winds raising dust into the atmosphere and redistributing it across the planet."
NASA Technical Reports Server (NTRS) 19910017768: Dust in the Mars atmosphere (1991)
[14] supported
During local dust storms, most suspended dust is confined below 20 km, whereas during larger storms, micron-sized particles can be mixed to higher altitudes.
"During local dust storms, most of the suspended dust comprising the storm is confined below 20 km. During larger dust storms, however, micron-sized dust particles may be mixed to higher altitudes."
NASA Technical Reports Server (NTRS) 19910017768: Dust in the Mars atmosphere (1991)
[15] supported
The suspended dust in the Martian atmosphere is dominated by igneous silicates containing more than 60% SiO2 or weathering products like clay minerals.
"Observed thermal IR spectra indicate that dust suspended in the atmosphere is a mixture dominated by igneous silicates containing mainly Si02 (> 60%), or by weathering P r odiict s such as clay minerals, perhaps with some basalt also present."
NASA Technical Reports Server (NTRS) 19910017768: Dust in the Mars atmosphere (1991)
[16] documented
The visual opacity of the Martian sky at Viking Lander sites never fell below a value of 0.1 during 1.25 Mars years of observation, indicating a persistent background dust haze.
"The opacity of the sky is best known at the two Viking Lan er sites, where the visual, vertical-column optical depth never fell below a valu tenths during the 1 and 1/4 Mars years of observations and yet exceeded 2-3 during two great dust storms in 1977."
NASA Technical Reports Server (NTRS) 19910017768: Dust in the Mars atmosphere (1991)
[17] supported
The proposed Mars colony power source is a nuclear fission surface power system with a total capacity of 1 MWel.
"To provide sufficient power, a nuclear fission surface power (FSP) system is proposed with a total capacity of 1 MWel."
Power Management and Distribution System for a Mars Surface Fission Power Reactor (2018)
[18] supported
NASA's Design Reference Architecture 5.0 describes fission surface power systems as enabling for human exploration of Mars.
"fission surface power systems (FSPS) are described as “enabling for the human exploration of Mars.”"
Mass Optimization of a Supercritical CO2 Brayton Cycle Power Conversion System for a Mars Surface Fission Power Reactor (2017)
[19] supported
A regenerative fuel cell that reuses a propellant tank recycled from the lander was found to have the best energy density and scalability of the storage options studied.
"A regenerative fuel cell using a propellant tank recycled from the lander was found to have the best energy density and scalability among all the options investigated."
Power Management and Distribution System for a Mars Surface Fission Power Reactor (2018)
[20] documented
The paper's preferred approach for a Mars or lunar fission reactor uses crew-assisted assembly and places the reactor in an excavated hole for radiation shielding.
"The preferred system implementation approach uses crew-assisted assembly and in-situ radiation shielding via installation of the reactor in an excavated hole."
A Comparison of Fission Power System Options for Lunar and Mars Surface Applications (2006)
[21] supported
The thermal energy reservoir has the worst storage efficiency but can be built using in situ resource utilization, making it a promising long-term option.
"The thermal energy reservoir, while having the worst storage efficiency, can be constructed through in situ resource utilization (ISRU), and is a promising long-term option."
Power Management and Distribution System for a Mars Surface Fission Power Reactor (2018)
[22] supported
The planned Mars surface power system uses three 333 kWe fission reactors with their conversion systems to supply a total of 1 MWe for 15 years, with the redundancy providing backup if one unit fails.
"For load following and redundancy purposes, the FSPS consists of three 333 kWe reactors and PCS to provide a total of 1 MWe for 15 years."
Mass Optimization of a Supercritical CO2 Brayton Cycle Power Conversion System for a Mars Surface Fission Power Reactor (2017)
[23] supported
Load-following scenarios studied include an extended dust storm, nighttime, daytime, and transient peak power operation, all accommodated by the system.
"Several main load-following scenarios are studied and accommodated, including an extended dust storm, nighttime, daytime, and transient peak power operation."
Power Management and Distribution System for a Mars Surface Fission Power Reactor (2018)
[24] supported
The optimal mass-minimized power conversion design is a supercritical CO2 Brayton cycle with 60% regeneration and two stages of intercooling.
"The optimal configuration is a sCO2 Brayton cycle with 60% regeneration and two stages of intercooling."
Mass Optimization of a Supercritical CO2 Brayton Cycle Power Conversion System for a Mars Surface Fission Power Reactor (2017)
[25] documented
A self-deployed, self-shielded fission system with its mobile power cart weighs about twice as much as the in-situ shielded system.
"The mass of a self-deployed, self-shielded fission system including the mobile PMAD cart was approximately twice that of the in-situ shielded system."
A Comparison of Fission Power System Options for Lunar and Mars Surface Applications (2006)
[26] supported
Power needs for human-tended Moon and Mars surface outposts are expected to be 25 to 100 kWe during early build-up phases.
"Power requirements for human-tended surface outposts and bases are expected to range from 25 to 100 kWe during the early build-up phases."
A Comparison of Fission Power System Options for Lunar and Mars Surface Applications (2006)
[27] supported
Nuclear fission systems are considered the most mass-efficient way to supply high power for surface missions.
"The most mass-efficient means of providing high power for surface missions is through the use of nuclear fission systems."
A Comparison of Fission Power System Options for Lunar and Mars Surface Applications (2006)