METRIC FLIGHTTHE ARLO / LUNAR PROGRAM
AI-generated concept of a compact lunar outpost with linked pressure modules, external solar arrays and radiators
THE ARLO · MOON STATION / 06

The lights stay on.
The heat gets out.

Generation, storage and thermal rejection are one engineering problem. Explore the consequences of a longer outage or a larger station load.

Explore the station ↗Read the design basis

AI-GENERATED CONCEPT ART · NO BUILT STATION CLAIMED

CHAPTER 06 / POWER & HEAT

A reference load, not a vendor specification

Concept study · 23 October 2026
Four crew / 30 days is a reference mission. Site, transport, safety case, mass budget and hardware remain open.

CHANGE THE ASSUMPTIONS / SEE THE CONSEQUENCES

How much is enough?

Nominal battery capacity2,000 kWh
Battery mass at illustrative 150 Wh/kg13.3 tonnes
Idealized effective radiating area48.4 m²

Storage = load × outage ÷ (0.90 efficiency × 0.80 usable fraction). Battery mass excludes reserve and environmental/aging penalties. Radiator assumes the same numerical heat load as electrical demand, emissivity 0.9, sink 3 K, no sunlight or terrain heating. Idealized values are not equipment selections. Sliders do not establish station feasibility.

ARLO ORIGINAL / ANIMATED EXPLAINER

Sunlight, storage and the long shadow

Read the film transcript

Solar generation serves essential loads and charges storage. During darkness, stored energy supplies the bus. Electrical demand becomes heat that must be rejected. At 20 kW and 72 hours the example needs 2,000 kWh nominal storage; the complete environment and reserves are not included.

Silent, captioned concept animation. Illustrates the design logic; does not depict built hardware or measured performance.

Power & heat: GENERATION, STORAGE, ESSENTIAL BUS, HEAT REJECTION; conceptual functional relationships
ARLO functional study 06 · conceptual relationships, not a construction drawing.

DESIGN NOTE 01

A reference load, not a vendor specification

The first power trade uses 20 kW average electrical demand and a provisional 30% allocation margin, giving 26 kW for planning. Actual loads must be built from equipment duty cycles, startup surges, EVA operations, science and contingency modes. Separate essential loads from equipment that can be shed. A single average cannot establish bus, inverter or cable sizing.

DESIGN NOTE 02

Darkness makes storage large

At 20 kW for 72 hours, delivered energy is 1,440 kWh. At 90% discharge-path efficiency and 80% usable depth of discharge, nominal battery capacity would be 2,000 kWh before aging, temperature effects and reserve. At an illustrative pack-level 150 Wh/kg, that is about 13.3 tonnes of batteries alone. These assumptions reveal why site choice, shorter crew visits, lower loads, fuel cells and eventual fission deserve a formal trade.

DESIGN NOTE 03

Solar first does not mean solar only

Tracking arrays need an illumination and shading model, dust allowances, thermal derating, deployment reliability and recharge time. To recover energy after a blackout, generation must serve the live load and charge storage. Fission is a credible development direction, but an ARLO reactor is neither procured nor qualified. No reactor output is counted as available station power.

DESIGN NOTE 04

Radiators close the energy balance

Most electricity used inside ultimately becomes heat. In vacuum, external heat rejection relies primarily on radiation. A screening model uses Q = emissivity × Stefan–Boltzmann constant × area × (radiator temperature⁴ − effective sink temperature⁴). The calculator assumes a cold idealized sink and emissivity 0.9. Real design must include terrain infrared, sunlight, view factors, dust, fluid loops and failure isolation; effective radiating area is not necessarily panel footprint.

Research behind this chapter

Sources checked 23 October 2026. ARLO-specific architecture and numbers are proposed assumptions. Public research references do not imply endorsement or partnership.

EDITION 15 · DESIGN STAGE

2 W mirror benchmark · no measured result · independent review and registration pending.

Current evidence and open actions ↗
EDITION 15 · DESIGN STAGE

2 W mirror benchmark · no measured result · independent review and registration pending.

Current evidence and open actions ↗
EDITION 15 · DESIGN STAGE

2 W mirror benchmark · no measured result · independent review and registration pending.

Current evidence and open actions ↗
EDITION 15 · DESIGN STAGE

2 W mirror benchmark · no measured result · independent review and registration pending.

Current evidence and open actions ↗
EDITION 15 · DESIGN STAGE

2 W mirror benchmark · no measured result · independent review and registration pending.

Current evidence and open actions ↗