EST · 2021
ENT/MSN-0 · RESEARCH BRIEF · 2026

The longest farm.

A research brief for rearing Tenebrio molitor beyond Earth: a low-mass, fast-cycle protein candidate worth testing carefully.

§A / The case
Why insects, off Earth

The smallest farm is still a hypothesis.

The promise is simple and unproven: a low-mass farm that eats difficult substrate and finishes fast. That is a research question before it is a mission plan.

A crewed Mars transit runs about 1,100 days. At a NASA-baseline protein intake of 0.8 g/kg/day, a four-person crew consumes roughly 235 kg of dry protein over the mission. Mass you would rather not launch. Every kilogram grown in-flight is a kilogram you do not lift off Earth's gravity well.

Tenebrio molitor is one of the more practical low-mass protein candidates studied for closed-loop systems. It converts substrate to body mass at 1.6:1, completes its rearing cycle in 80 days, and is 52% protein on a dry basis. It needs little water and less space, and it tolerates the cramped, variable conditions a spacecraft actually offers, but every one of those assumptions needs controlled testing.

Crucially, mealworms metabolise lignocellulosic waste: the inedible plant matter a closed-loop habitat already produces. The frass they leave behind is a clean substrate for plant growth. Feed in the waste stream, harvest protein, return the residue to the garden: the loop might close, if the biology behaves under mission constraints.

That advantage compounds with distance, but the numbers are scenario models, not flight claims. In low Earth orbit the case is weak because resupply is available. On the lunar surface and Mars transit, where resupply becomes harder, the question becomes worth testing seriously.

§B / Profiles
Three destinations

One protocol, three gravities.

MISSION PROFILE · 01 ENT/MSN-01

LEOLow Earth Orbit · ISS-class

ENT-MSN-1
Duration
30–180 d
Crew
4–7
Δv from Earth
9.4 km/s
Protein demand
~6 kg dry/wk
Reared in-situ
10–30%
Mass saved
~120 kg / 180d
Tech readiness
TRL 4, payload
MISSION PROFILE · 02 ENT/MSN-02

MOONLunar surface base

EARTH LUNA 384,400 km
Duration
14 d – 12 mo
Crew
4–8
Gravity
0.166 g
Resupply cadence
60–180 d
Reared in-situ
40–70%
Substrate
Algae + waste
Tech readiness
TRL 3, concept
MISSION PROFILE · 03 ENT/MSN-03

MARSTransit + surface, conjunction-class

EARTH MARS Δv ≈ 4.3 km/s · 7 mo transit
Duration
≥ 1,100 d
Crew
4–6
Gravity
0.38 g (surface)
Comms latency
4–24 min
Reared in-situ
≥ 80%
Closed loop
Required
Tech readiness
TRL 2, research
§C / Prior art
What we bring

We don't fly payloads. We test the husbandry.

Bioregenerative life support is not new. ESA's MELiSSA loop and Beihang University's Lunar Palace 1 have spent decades proving that closed ecological systems can sustain crews. What the field lacks is a production-grade insect protocol: husbandry that survives contact with a real operation rather than a sealed experiment.

That is the gap Entolab can help narrow. We bring five years of T. molitor husbandry in working rooms and a private-beta software stack for batch-level insect operations, the same records discipline we use on terrestrial batches.

The brief is meant to shape rearing protocols, microgravity tolerance studies, and integrated bioregenerative life-support architecture questions with academic and payload partners. We contribute terrestrial husbandry and record structure; partners contribute the science questions and, eventually, test opportunities.

PRIOR ART · ESA MELiSSA · BEIHANG LUNAR PALACE 1 · OONINCX 2015 · KATAYAMA & TAKO 2018 · ENTOLAB INTERNAL 2024–26

§D / Contact
Research brief

Partner conversations, 2026.

We are shaping a research brief for partners interested in insect rearing beyond Earth: university labs, payload integrators, and PhD candidates with a relevant question. Conversations begin 15 September 2026.