LifeSupportCalc


Mission

Crew size
LED persons


Mission duration
LED days


Consumables reserve
LED percent


Activity profile
LED

metabolic multiplier water multiplier

Food and Water

Food mode
LED

edible food kg/crew-day packaging kg/crew-day cold fraction

Water recycling
Water LED

total water recovery percent subsystem power kW per four crew

Medical or event water reserve
LED kg total


Atmosphere Revitalization

Oxygen supply
LED

electrolysis? kWh/kg O2 consumable kg/kg O2

Emergency O2 backup for electrolysis mode
LED days


CO2 scrubber
CO2 LED

capture percent kW per four crew sorbent kg/kg CO2 filters kg/crew-day

CO2 reduction and oxygen-loop closure
LED

reduced CO2 percent kW per four crew

Waste, Power and Habitable Volume

Power source
Power LED

kg/kW electric kg/kWh storage

General electrical loads
LED hotel/load kW trace cleanup kW waste kW per four crew


Countermeasure and thermal loads
LED exercise equipment kW thermal control kW power margin percent


Power storage duration
LED hours


Living space model
Volume LED deck height m

net habitable volume m3/crew

Artificial Gravity

Artificial-gravity mode
AG LED

radius m floor gravity g

recalculate  |  reset nominal

Results

Results will appear here.

LED Key

red down triangle The value is too high, too low or operationally unsafe for the selected mission.

yellow down triangle The value is probably workable only with adaptation, redundancy or engineering changes.

green circle The value is inside the simple comfort or closure zone for this preliminary model.

yellow warning triangle The value may be too low for immediate comfort, health protection or closed-loop operation.

red up triangle The value is too low for the selected mission unless another subsystem covers it.

About the Calculator

LifeSupportCalc is a preliminary sizing tool for crewed spacecraft and habitats. It estimates food, water, oxygen, carbon dioxide removal, water recycling, solid waste storage, power generation, thermal rejection, net habitable volume and artificial-gravity spin requirements.

The calculation is a mass-balance model, not a flight-certified ECLSS design. It uses published baseline assumptions where possible, then exposes the uncertain engineering values as inputs. The defaults are deliberately editable because spacecraft life support depends on the vehicle architecture, redundancy philosophy, crew workload, hygiene policy, mission phase, storage method, venting policy and maintenance plan.

Main Equations

SubsystemEquation or rule
OxygenO2 = crew-days x O2 per crew-day x activity multiplier. Electrolysis feed water = O2 x 18/16.
CO2CO2 = crew-days x CO2 per crew-day x activity multiplier. Regenerable scrubbers remove CO2 without bulk sorbent replacement. LiOH mode carries expendable sorbent.
SabatierCO2 + 4H2 -> CH4 + 2H2O. Water returned = reduced CO2 x 36/44. Methane vented = reduced CO2 x 16/44.
WaterMakeup water = potable plus hygiene plus net O2-generation water minus recovered wastewater, with reserves added to stored makeup.
PowerAverage power is the sum of subsystem, hotel, thermal, trace-contaminant, exercise and waste-management loads, multiplied by the selected margin.
Artificial gravityAcceleration = omega squared x radius. Spin rpm = 60/(2*pi) x square-root(acceleration/radius). Tangential speed = omega x radius.

Health Interpretation

For short missions, microgravity may be acceptable with exercise and recovery planning. For missions of many weeks to months, the calculator flags artificial gravity or intensive countermeasures because microgravity affects weight-bearing bone, skeletal muscle, cardiovascular regulation, sensorimotor control and neuro-ocular risk. The correct artificial-gravity dose is still not settled. A rotating habitat may reduce risk, but radius, rpm, Coriolis forces, interior layout, exercise, sleep, and partial-gravity exposure time all matter.

Default Human Metabolic Values

ParameterDefaultUnit
Oxygen consumed0.816kg per crew-day
Carbon dioxide produced1.04kg per crew-day
Edible food1.51kg per crew-day
Food packaging0.262kg per crew-day
Potable water2.50kg per crew-day
Personal hygiene water0.40kg per crew-day
Urine water1.62kg per crew-day
Humidity condensate from respiration and perspiration1.90kg per crew-day
Crew solid waste allowance1.00kg per crew-day
Life-support waste allowance0.50kg per crew-day

References

Anderson, Molly S., Ewert, Michael K., Keener, John F. and Wagner, Steven A. (2018). Life Support Baseline Values and Assumptions Document, NASA/TP-2015-218570/REV1. NASA Technical Reports Server.

NASA (2025). Environmental Control and Life Support Systems (ECLSS). NASA Marshall Space Flight Center.

NASA (2023). NASA Achieves Water Recovery Milestone on International Space Station. NASA.

European Space Agency. Advanced Closed Loop System. ESA.

NASA Office of the Chief Health and Medical Officer (2023). NASA-STD-3001, Volume 2, Human Factors, Habitability, and Environmental Health. NASA Human System Standards.

Clément, Gilles R., Bukley, Angelia P. and Paloski, William H. (2015). Artificial gravity as a countermeasure for mitigating physiological deconditioning during long-duration space missions. Frontiers in Systems Neuroscience. Frontiers.

Man, Joey, Graham, Taylor, Squires-Donelly, Georgina, et al. (2022). The effects of microgravity on bone structure and function. npj Microgravity. Nature.

Hall, Theodore W. (2000 to 2018). SpinCalc, an artificial-gravity calculator in JavaScript. artificial-gravity.com.


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