2010
DOI: 10.1016/j.actaastro.2009.10.027
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Concept of a Lunar FARM: Food and revitalization module

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Cited by 9 publications
(3 citation statements)
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“…The food and revitalisation module (FARM) greenhouse of 528 m 2 implementing a range of 21 crops supplies 100% of human nutritional requirements for 18 astronauts [ 92 ]. A simulated bioregenerative life support system supplemented by physicochemical methods (for atmospheric recycling, water recycling, waste reclamation and food production) with 15 types of hydroponic crop, silkworm husbandry and both solid and liquid waste recovery yielded 29.7 kg of oxygen, potable and hygiene water and food at 2700 calories/person/day (375.5 g carbohydrate, 99.5 g protein and 91.2 g fat) with 99.4% material closure [ 93 ].…”
Section: Discussionmentioning
confidence: 99%
“…The food and revitalisation module (FARM) greenhouse of 528 m 2 implementing a range of 21 crops supplies 100% of human nutritional requirements for 18 astronauts [ 92 ]. A simulated bioregenerative life support system supplemented by physicochemical methods (for atmospheric recycling, water recycling, waste reclamation and food production) with 15 types of hydroponic crop, silkworm husbandry and both solid and liquid waste recovery yielded 29.7 kg of oxygen, potable and hygiene water and food at 2700 calories/person/day (375.5 g carbohydrate, 99.5 g protein and 91.2 g fat) with 99.4% material closure [ 93 ].…”
Section: Discussionmentioning
confidence: 99%
“…Some design studies for future Lunar or Martian bases 10,11 consider the use of deployable structures to reduce its mass and the volume occupied inside the launch and transfer vehicles. Such greenhouse modules arrive at the destination in a folded or packaged configuration and have to be unfolded and deployed before the first seedlings can be planted in the grow area.…”
Section: Start-up Phasementioning
confidence: 99%
“…Finetto et al [42] consider rigid and hybrid cylindrical structure concepts for the Lunar Food and Revitalization Module (FARM) which would be part of a Permanent Human mOon Exploration BasE (PHOEBE). The rigid cylinder has a diameter of 8 m, a length of 12 m and at the end caps there are 1 m spherical caps, similar to the (deployed) hybrid design, but suffers from higher mass.…”
Section: (Semi-)cylindersmentioning
confidence: 99%