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STELLAROrbital computing
Node-3 / Roadmap / Mission 3

Node-3: The first STELLAR orbital cluster

Node-3 introduces multi-node operations: workload distribution, node-to-node replication, failover, and orbital resource scheduling across more than one data-center asset.
Multi-node
Topology
Failover
Primary proof
Replication
Advances
Node-3/ visual
Inter-satellite relay node in formation flight
From single node to clustered infrastructure.

Two coordinated nodes. Workload distribution. Replication. Failover. The shift from "satellite" to "infrastructure".

01 / mission narrative

Why this mission, and what it must prove

Demonstrate that orbital data centers become more valuable when they operate as a coordinated infrastructure layer instead of isolated satellites.

01 / The infrastructure thesis

A satellite is a product. A cluster is a network

A single orbital node is impressive engineering. A coordinated cluster is a different category workloads can move across nodes by contact opportunity, by thermal margin, by customer policy. Node-3 is the first STELLAR mission that operates as more than one spacecraft. It is the moment "orbital data center" stops being a metaphor.

02 / What changes

Scheduling, replication, failover across orbits

A workload submitted to Node-3 isn’t pinned to a specific spacecraft. The scheduler chooses the node with the best joint state power, thermal, contact, and locality of input data and replicates results across nodes for delivery resilience. If a node enters safe-mode, in-flight jobs and stored products fail over to a peer.

03 / The new operating model

One service. Two spacecraft. Coordinated in orbit

Node-3 keeps the Node-2 customer contract surface same API, same SLAs but the implementation underneath is now distributed. Customers don’t see the complexity; they see better delivery times and a service that survives a single-node degradation. Operations sees two spacecraft, one cluster health view, one reconciliation log.

02 / mission profile

Orbit, payload, power, thermal, comms, partners

The profile is the mission’s physical truth every architectural choice descends from these numbers.

Orbit
Co-planar 500–550 km, phased 180° apart
Altitude
500–550 km
Inclination
~55° (matched per launch)
Operational duration
36-month cluster operating window
Payload class
Two coordinated dedicated modules 200 kg each
Power envelope
1.8 kW peak per node
Thermal envelope
1.6 kW peak heat rejection per node
Contact window
14–22 passes/day combined cluster contact
Primary partners
Two spacecraft prime contracts (or one dual-launch) · Inter-satellite link (ISL) provider RF backbone · Expanded multi-site ground network · Commercial customers with cross-region resilience needs
03 / technical architecture

Systems that must work as one

The mission is the sum of these subsystems and the way they constrain each other.

SystemSpecificationDesign note
Cluster schedulerJoint-state scheduler power, thermal, contact, localityPicks the node best suited to a workload by joint orbital state and customer policy. Failover-aware: in-flight jobs migrate when a peer node degrades.
Inter-node linkRF inter-satellite link (Ka-band class)Carries replication traffic, cluster heartbeats, and cross-node command authorization. Optical relay is staged for Node-5; Node-3 uses RF for risk-reduction.
Replication storageCross-node mirrored pools, customer-policy-drivenCustomer policy chooses replication: local-only, cluster-mirrored, or quorum-of-N. Hash-chain integrity preserved across nodes.
Cluster health modelSingle ground-cloud view of two-node stateOperations and customer dashboards show cluster state power, thermal, contact, queue depth, replication lag, SLA budget as a single coordinated view.
Cross-node receiptsQuorum-signed delivery evidenceDelivery is acknowledged when N-of-M nodes have signed the result. Lets the customer verify that no single spacecraft owns the truth.
04 / capabilities added

What this mission adds to the roadmap

Each mission is justified by a specific new capability not just a larger payload.

Capability 01

Workload distribution across more than one orbital node

Capability 02

Replication and failover for selected datasets

Capability 03

Resource scheduling across power, contact, thermal, and storage constraints

Capability 04

Cluster health model visible to ground-cloud operations

Capability 05

Cross-node delivery reconciliation with quorum receipts

Capability 06

Customer-policy controls for replication, residency, and durability

05 / phased plan

Mission timeline milestones, not vibes

The plan is broken into reviewable phases. Each phase ends in a deliverable a stakeholder can read.

Phase 0Concurrent with Node-2 ops
Cluster architecture review

Scheduler protocol, replication policy model, ISL contract, and ground-cloud cluster view defined.

Phase 1TBD
Node-3a launch

First cluster member launched. Operates standalone (Node-2-class) until Node-3b joins; pre-flight verifies ISL acquisition.

Phase 2~Node-3a +6 months
Node-3b launch + cluster join

Second member launched; ISL acquisition; cluster scheduler activated; first cross-node workload migration.

Phase 336-month window
Operational cluster service

Steady-state cluster operation. Replication, failover, quorum delivery exercised under live customer load.

06 / risk register

What is closed, mitigated, in design, or open

A serious mission tracks risks honestly. Closed, mitigated, in design, and open items are listed without softening.

RiskStateDescription
ISL link availability and latencyIn designRF inter-satellite link availability windows drive replication lag. Node-3 architecture must tolerate multi-orbit ISL gaps without breaking customer SLAs.
Split-brain on partial connectivityIn designCluster scheduler must avoid double-execution under transient ISL loss. Resolved through quorum protocols and ground-mediated tiebreak.
Operations cognitive loadMitigatedCluster health view collapses two-node state into one operator workflow. Validated against synthetic split-brain scenarios in GroundLab.
Coupled launch dependencyOpenA coordinated cluster requires two functioning nodes. Risk is mitigated by staggered launches: Node-3a flies as standalone Node-2.5 if Node-3b slips.
07 / verification

Every claim ties to an evidence product

The right way to read a mission page: claim → evidence → state. If a row is in the wrong state, the page is what is broken not the program.

ClaimEvidenceState
Workload migrates across nodes without customer-visible SLA breach.Cluster scheduler log + customer SLA reconciliationPlanned
Stored products survive one-node safe-mode without loss.Quorum receipt chain + replication lag telemetryPlanned
ISL link maintains contracted replication budget.On-orbit ISL availability vs. mission baselinePlanned
Operations workflow stays single-pane under two-node state.Operator usability + incident-response playbook executionDraft
From single node to clustered infrastructure.
Advancement
Node-3
Stage
Roadmap
Program state
09 / continuity

What this mission inherits, what it enables

Each mission is a step on a single staircase. These bridges spell out what comes from the prior step and what becomes possible after.

Roadmap / index

All STELLAR missions

Open roadmap

Continue to Node-4: Sovereign Orbital Region

Node-3 builds on Node-2 by moving from "From payload validation to early commercial service." toward "From single node to clustered infrastructure.".