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Evidence & Trust
Develop space and aerospace systems through simulation, evidence, prototype and qualification-readiness gates.
IYABOKO Space & Aerospace connects mission architecture, digital twins, telemetry, sustainable infrastructure, software and prototype preparation with Sentinel assurance and accountable specialist handoff.
Disturb the simulated mission. Watch the evidence and assurance state respond.
SpaceCore is IYABOKO’s evidence-centred space-systems engineering demonstrator. The IOSTS-R Live Mission connects browser-generated telemetry, digital-twin state, configuration context, verification evidence, Sentinel assurance and accountable human decision gates.
IYABOKO Spacecraft Live Demonstrator
IOSTS-R research spacecraft simulation with evidence-centred SpaceCore assurance.
LOW EARTH ORBIT SIMULATION
SpaceCore Assurance
SpaceCore shows what has been demonstrated, what changed, what evidence exists, and which human decision remains.
Live Demonstration Controls
Engineering Event Stream
Digital Twin State
The intergalactic profile is intentionally treated as experimental research. Speculative physics cannot be promoted to demonstrated engineering evidence without falsifiable, reproducible evidence.
This interface is a simulated IYABOKO / IOSTS spacecraft demonstrator. The spacecraft image is a conceptual visualization. The telemetry is generated in the visitor’s browser and is not received from a physical spacecraft. IOSTS-X represents speculative future-physics research and is not presented as demonstrated intergalactic propulsion.
Flight Authority: NONE
Explore the simulated spacecraft, Solar System, galaxy and exoplanet reference space in one governed live lab.
This second live demonstrator extends the existing IOSTS-R / IOSTS-X spacecraft demonstrator with a multi-scale cosmic visualisation, adaptive level-of-detail rendering and a read-only SpaceCore scientific-reference plane. IOSTS telemetry remains simulated; external catalogue and ephemeris information remains separately labelled as reference evidence.
Procedural stars and galaxy structures are visualisation data, not a complete observed catalogue. No physical spacecraft, radio, propulsion, HIL actuator or flight computer is controlled by this interface. Flight Authority: NONE.
FlightCore-1 Physical Demonstrator Programme
Explore the reaction-wheel F1 laboratory design and P0 passive measurement study. These are preliminary engineering concepts, not live spacecraft hardware or real-time telemetry.
Reaction Wheel F1 — Physical Prototype Review
Photorealistic concept imagery, CAD geometry, and preliminary documentation for engineering review. No physical hardware has been assembled or tested.
Physical Demonstrator Design
Proposed N20 brushed DC motor, TB6612FNG driver, Arduino Nano, lid interlock, local motor power cutoff, and time-limited pulse tests. Component selection, rotor retention, and protective enclosure still require validation.
Concept imagery · NOT BUILT
Parametric Enclosure Geometry
OpenSCAD models, base/lid STL files, and dimensional references are included for preliminary fit checks. The CAD preview does not certify rotor containment or mechanical tolerances.
CAD render · FIT-CHECK ONLY
Passive Measurement Study
Passive load-cell measurement study, uncertainty analysis, and synthetic data simulation. No active propulsion engine or experimentally verified thrust is represented.
Study only · NO ENGINE FIRINGFLIGHTCORE-1 · 7 governed engineering work packages reported as PREPARED.
HOLD — requires independent per-engine/tenant verification.
BOM + rotor retention + current limits + emergency isolation + technician sign-off.
All images are concept visualisations or CAD renderings, not photos of built hardware. No real-time data feed. Sentinel production release remains independent.
Use C3 for governed computational analysis before mission evidence progresses through SpaceCore and Sentinel.
In the late-August architecture, C3 Live Computer became the general governed computational demonstrator, while SpaceCore remained the evidence-centred mission demonstrator for the Space & Aerospace sector and IOSTS-R.
Governed Compute Runtime
IYA-24 reference runtime, domain validation, adaptive continuity, HIL qualification and evidence-oriented compute routing.
Mission Evidence Runtime
Telemetry, digital-twin state, verification evidence, Sentinel assurance and accountable human mission-review gates.
Controlled Deployment Candidate
Late-August C3 commercial packaging remained bounded to simulation authority with direct physical actuation disabled.
Power on C3. Watch a problem become evidence, simulation and a traceable computational decision.
IYABOKO C3 Live Computer is the public interactive demonstration layer for the C3 governed computational architecture. Visitors can frame a scientific or technical problem, simulate evidence intake, inspect anomaly and transition analysis, compare CPU/GPU/FPGA/quantum-simulator suitability, and see Sentinel and KEGEPA preserve uncertainty and decision boundaries.
C3 canonical runtime v2.9.0 · C3 Computer Commercial v1.2.0 Production Candidate · authority ceiling O0 simulation · direct actuation OFF.
From server simulation toward a governed FlatSat / HIL laboratory demonstrator.
The August programme pathway progressed beyond browser-only simulation planning into a controlled hardware-backed research track while keeping flight authority, launch authority and public hardware command disabled.
SpaceCore C3 Native Integration
Mission-simulation analysis, evidence packaging, IYA-24/Sentinel registries and governed C3 compute support.
IOSTS-R HIL-1
Low-voltage bench electronics, sensors, safe-state logic, fault injection and signed observed telemetry for laboratory research.
Read-only Live Mission
Validated HIL telemetry may be displayed publicly only after the commissioning gate. No anonymous hardware-command route is provided.
Qualification is not granted and flight authority remains NONE. A live simulation or hardware-backed HIL demonstration is not a qualified spacecraft system.
Space development programmes.
Use simulation and evidence before higher-cost or higher-consequence physical progression.
Mission Architecture
Objectives, phases, interfaces, constraints, failure logic and evidence structure.
Digital Twin & Telemetry
Orbit, subsystem, telemetry and scenario modelling before physical integration.
FlightCore / Subsystem Demonstrators
Controlled software and hardware prototypes with explicit maturity limits.
Orbital Sustainability
Debris awareness, servicing concepts and controlled recovery/deorbit research.
Verification Readiness
Requirements, QRM, test planning, SIL/MIL/HIL preparation and specialist handoff.
Sentinel Space
Risk, evidence, findings, remediation, dependencies and review gates.
Progress toward qualification through evidence.
Flight or mission claims should be matched to the specific evidence and external authority required.
Define
Mission boundary.
Model
Digital simulation.
Assure
Sentinel review.
Prototype
Controlled build.
Verify
Bench/SIL/MIL/HIL.
Review
Qualified external gate.
Space authority boundary.
IYABOKO Space & Aerospace supports research, simulation, software, architecture and prototype preparation. It does not claim flight certification, launch authority, operational debris recovery or crewed-system safety without qualified engineering, testing and relevant authorities.
Simulation & prototype
IYABOKO can build controlled evidence and demonstrators.
Qualification & certification
Required specialists and authorities control consequential release decisions.
No maturity shortcut
A live simulation is not flight evidence and a prototype is not a qualified spacecraft system.
Build the next space evidence gate.
Move from mission concept to controlled simulation, verification readiness or research partnership.