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CONSTANELLIS-ARS-01·ATLAS-C / HERMES CISLUNAR LOGISTICS·TARGET — 89.5°S · SHACKLETON RIM SECTOR·NEXUS-L4 COMMUNICATIONS RELAY ACTIVE·CAGE CODE: 8RUU8 · ITAR REGISTERED · 8(a) CERTIFIED·LUNAR INFRASTRUCTURE PROGRAM — DEVELOPMENT PHASE·IL-4+ CLEARANCE PATHWAY ACTIVE·CONSTANELLIS-ARS-01·ATLAS-C / HERMES CISLUNAR LOGISTICS·TARGET — 89.5°S · SHACKLETON RIM SECTOR·NEXUS-L4 COMMUNICATIONS RELAY ACTIVE·CAGE CODE: 8RUU8 · ITAR REGISTERED · 8(a) CERTIFIED·LUNAR INFRASTRUCTURE PROGRAM — DEVELOPMENT PHASE·IL-4+ CLEARANCE PATHWAY ACTIVE·
2026.03.30
Surface Parameters
TerrainRegolith / Basalt
Elev Delta2,340 m
Night Dur.354 hrs
Temp Range−173°C → 127°C
ICE DepositsConfirmed
Map Res.<1 m
Mission Architecture
DesignationARS-LI-01
Primary Veh.ATLAS-C
RelayHERMES OMV
CommsNEXUS-L4
Target89.5°S
CLPS Window2027–2030
Shackleton Crater
Primary ATLAS-C Target Zone
89.9°S / 0.0°E
Haworth Crater
Secondary Ops Zone
87.5°S / 351.0°E
Nobile Crater
Ice-Rich Survey Area
85.2°S / 53.5°E
PRIMARY TARGET ZONE
Lunar Infrastructure Program

The explorer's job is to come back with coordinates.

The Moon has been mapped. The resources have been catalogued. The coordinates exist. What comes next is not exploration — it is development.

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842 lbs
Samples returned by Apollo
Sub-meter
Surface map resolution
Confirmed
Polar water ice deposits
2027–2030
ATLAS-C mission window

01 — Coordinates

Water where the Sun never shines.

Between 1959 and 1976, ninety missions produced a dataset no one has fully acted on. LCROSS confirmed it definitively: the permanently shadowed regions of the lunar south pole hold approximately 3.5 billion tonnes of water ice. The mission data is not in dispute. The infrastructure to reach it does not yet exist.

Shackleton Crater sits at 89.9°S — 2,100 metres deep, temperatures permanently below −163°C, sunlight on the rim 89% of the time. It is the optimal site for a permanent human outpost. ATLAS-C targets it first.

The exploration chapter is closed. Constanellis was founded to open the development chapter — systematically, from the ground up, with the right customers already engaged.

PSR Survey Data

Ice Reserves~3.5 billion tonnes
Primary TargetShackleton — 89.9°S
Crater Depth2,100 m
PSR Temp−163°C (min)
Rim Sunlight89% of lunar day
Target Sites4 confirmed PSRs
Survey SourceLCROSS · LRO · M³

"The first organization to deploy infrastructure into the PSRs doesn't just participate in the lunar economy. It defines the terms on which everyone else operates."

02 — Platform

ATLAS-C

Advanced Terrain-Landing Autonomous System — Class C

ATLAS-C is the foundational delivery platform for the Constanellis Lunar Infrastructure Program. Designed from first principles to survive the 354-hour lunar night, ATLAS-C enables sustained surface operations where no lander has ever operated continuously.

Tower Mode deploys a 4.2-metre mast to maintain line-of-sight communications across PSR terrain. Terrain-Relative Navigation delivers a 1.1-metre circular error probable — precision required for infrastructure-class cargo.

NIGHT SURVIVAL
Dual RTG + Primary Li
CLPS COMPLIANT
NASA Task Order Ready
ATLAS-C Specifications
Wet Mass842 kg
Dry Mass406 kg
Payload Cap.112 kg
Power Output280 W continuous
Night SurvivalDual RTG + primary Li
Temp Rating−173°C certified
GNC Accuracy1.1 m CEP
Tower Mode4.2 m deployable mast
CommsS-band + NEXUS-L4
Mission Window2027–2030 (CLPS)

03 — Orbital Vehicle

HERMES OMV

High-efficiency Relay and Maneuvering Execution System — Orbital Maneuvering Vehicle

HERMES Specifications
PropellantMMH / NTO bipropellant
Engine Isp312 s
ΔV Budget1,240 m/s
Payload Bay220 kg
Primary Orbit100 km circular
PSR ApproachTLI → LLO → descent
Relay Downlink622 Mbps hybrid
Station Life3 years / 12 orbits

HERMES is the cislunar logistics backbone. Designed for lunar orbit insertion, payload deployment, and sustained orbital relay service, HERMES keeps ATLAS-C connected to Earth and positions payloads for south pole approach with precision.

As an orbital relay node, HERMES provides 622 Mbps hybrid S-band and optical communications — sufficient for full-resolution surface imaging and NEXUS real-time data downlink across the PSR network.

The HERMES platform is dual-use: civil CLPS relay operations in the 2027 window, followed by classified payload hosting under USSF and IC task orders beginning 2029.

04 — Infrastructure

The Wires

Wireless Infrastructure for Remote Exploration Systems

The gap between exploration and development is not a knowledge gap. It is an infrastructure gap. Every government and commercial actor planning lunar operations faces the same problem: there is nowhere to plug in.

WIRES delivers the foundational utility layer — power distribution, broadband relay, and precision navigation — that every subsequent lunar operator requires. The organization that builds this layer collects tolls from everyone who uses it.

01
THE FACTORY
Precision manufacturing · flight-qualified components
02
THE BRAIN
NEXUS AI platform · FORGE hardware systems
03
THE TRUCKS
ATLAS-C lander · HERMES cislunar OMV
04
THE WIRES
Power · Communications · PNT · cislunar utility
WIRES Infrastructure Specs
Optical Relay622 Mbps S-band / optical
Earth Latency340 ms (relay)
Power Grid5 kW distributed
RTG BackupRadioisotope failsafe
PNT Sats12-satellite lunar orbit
PNT Accuracy8 m position (1σ)
Ground SegmentIL-4 cleared facility
NEXUS LinkedFull fusion integration

05 — Data Platform

NEXUS

Neural EXploration Unified System — multi-INT lunar intelligence platform

NEXUS is the ground-side intelligence layer that turns raw lunar sensor data into actionable information. Operating at IL-5/IL-6 classification, NEXUS fuses multi-source inputs — SAR, EO, hyperspectral, PNT — and delivers fused products to NASA, USSF, the IC community, and qualified commercial operators in real time.

The platform is built for defense integration from first principles. Outputs are delivered in NITF 2.1, GeoTIFF, SICD, and via direct API — compatible with existing IC and USSF exploitation infrastructure without translation layers.

NASA
Civil mission data products
USSF
Cislunar domain awareness
IC Community
IL-5/IL-6 fused intel
Commercial
API-delivered survey data
NEXUS Platform Specifications
ClassificationIL-5 / IL-6 capable
Sensor FusionSAR · EO · HSI · PNT
ProcessingReal-time, classified cloud
Latency<340 ms Earth relay
Output FormatsGeoTIFF · NITF 2.1 · SICD
API AccessAuthenticated REST / STIX
ArchiveFull-mission data retention
DeliveryJWICS · SIPRNet · unclass

The mission begins
with a conversation.

Whether you represent a government program office, a commercial mission operator, or an institutional investor — the infrastructure layer is being built now. This is the conversation to have before the window closes.