Table 1 Constraints on past and current experimental platforms including small satellites, space stations, rovers, planned lunar habitation, and martian habitation.
Platform | Volume | Power | Op. lifetime | Temperature | Air comp. |
---|---|---|---|---|---|
CubeSat | 0.0187 m3 | 20–45 W | ~20 years | Requires heating unit within constraints | Self-contained |
PocketQube | 0.000125 m3 | Variable | ~5 years | ||
Bioculture System | Not stated | 140 W | ~60 days | 37–45 °C in main chamber, ambient to 5C in cooling chamber | Self-contained medical grade gas |
WetLab-2 (SmartCycler) | 235.97 m3 | 350 W | Extractions <3 h, no lifetime stated | 50–95 °C | None, reliant on cabin air system |
Rodent Habitat Hardware System | 0.019 m3 | Not stated | ~30 day experiments | Ambient temp, no heating module | |
Compact Science Experiment Module | 0.0015 m3 | 3.2 W | >1 month experiments | ||
Vegetable Production System (Veggie) | 0.48 m3 growth area | Not stated | >12 day experiments, can replace crops | ||
Advanced Plant Habitat (APH) | 889.44 m3 growth area | ~1 year | 18–30 °C | Self-contained gas supply | |
Spectrum | 10 × 12.7 cm internal area | 12 day experiments | 18–37 °C | None, reliant on cabin air comp | |
BRIC-60 | 11.03 m3 | Unpowered | >12 day experiments | Ambient temp, no heating module | 60 M variant can draw from an external gas tank |
BRIC-100 | 38.78 m3 | Self-contained gas canister of designated composition | |||
BRIC-100VC | 16.33 m3 | 4.5 months | |||
KSC Fixation Tubes (KFTs) | 0.2387 m3 | 67 days | |||
miniPCR | 0.00066 m3 | 65 W | ~2 year | <120 °C | Airtight, reliant on cabin air comp |
Group Activation Pack-Fluid Processing Apparatus (GAP-FPA) | Eight 6.5 cm3 test tubes | Unpowered for manual | Not stated | 4–37 °C | |
Multi-use Variable-g Platform (MVP) | Twelve 800 cm3 modules | Not stated | 14–40 °C | ||
MinION | 0.0796 m3 | 5 W | ~1 year | Ambient temp, no heating module | |
Perseverance (MOXIE) | 0.017 m3 | 300 W | ~2 years | 800 °C operational −60 °C ambient | CO2 input CH4 output |
Gateway (HALO) | >125 m3 planned internal volume | ~60 kW | >2 years | ~18 °C | Pressurized cabin air |
Mars Hab (6 Crew) | 300 m3 | ~100 kW | 600 day nominal, 619 day maximum | ~18 °C | Pressurized cabin air |