ZENIT Space
Program reference · R2 · 29 October 2026. Enable JavaScript for search, architecture views and the factbook.
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Qi Vanguard Fleet
A coordinated expedition architecture with Zorak, research vessels, carriers and interceptors.
Design canon · Sources S4, C1, S6
- Crewed vessels: 14
- Major vessels: 6
- Interceptors: 8
- Drone allocation: 62 across 3 hosts
- Outverse fit: Three-layer design across all 14 vessels
- Flight design baseline: 24 July 2026
- Routine cruise: 0.01c (≈2,998 km/s)
- Rapid formation cruise: 0.05c (≈14,990 km/s)
- Maximum sustained formation cruise: 0.075c (≈22,484 km/s)
- Emergency sprint: 0.10c (≈29,979 km/s)
Zorak is the flagship. Fronak and Anorak are research vessels. Derko, Herko and Sorko are carriers, each with two assigned interceptor docks.
Design ratings for the six major vessels travelling in formation with all eight interceptors docked. Emergency sprint is a short-duration setting.
The fleet adopts the three-layer Outverse design with sector burst reserves, SERAT recovery and hull damage mapping. Five functions per layer each have a qualification check. Zorak supplies the full-capacity sector reference. Each ship must qualify its own sector limits and simultaneous cooling budget.
The eight interceptors conserve reserve by remaining docked during transmission and cruise in the working doctrine. All fleet entries are conceptual design records, not live operational status.
Vessel Power & Propulsion
Two protected source lanes feed separated SERAT trunks and the conceptual propulsion stage.
Concept · Sources S1, S4, C1
- Chamber-order reference: QVCO-R1
- Source protection: Local Fuse A / B
- Central chamber: Two protected lanes
Main chain: Fusion A/B → Local Fuse A/B → Central Bidirectional Fuse → SERAT Power Corridor → Vector Accelerator → Main propulsion.
Each major vessel has two separate stern propulsion assemblies for forward thrust. Hull manoeuvring thrusters handle attitude and formation corrections.
CMC reference, GENI control, system buses, gravity control, shielding, cooling and other vessel loads sit alongside or branch from the energy architecture. A diagram is not proof of propulsion performance.
CMC & Vessel Reference
A separate reference and synchronization system near the vessel centre of mass.
Concept · Sources S1, S4, C1
- CMC: Central Magnetic Core
- Anorak reference: CRB-1 near station 55
- Anorak hull concept: 420 × 96 × 72 m
CMC is not the fusion reactor and is not drawn around it. The architecture separates reference, synchronization and compensation from power generation.
The Anorak hull and station reference are working project context. The underlying dimensional specification was not loaded.
Outverse & Aurora Shield
Aurora Shield’s Outverse mode is a 15-region concept for the Qi Vanguard Fleet, with five functional regions in each of three main layers.
Speculative concept · Sources S6, C1, S4
- Shield mode: Outverse · Space
- Fleet layout: 3 main layers × 5 functional regions
- L3 · Outer protection: GENI-10 first contact, debris deflection and sector burst reserve
- L2 · Middle recovery: SERAT load distribution, heat buffering and cooling
- L1 · Inner hull mapping: Impact location, damage sensing and evidence checks
Each region has a defined job and a pass check in the 3 × 5 function map. The functions share the active sector’s work, impulse and cooling limits.
Zorak’s single-sector simulation supplies the reference targets. Each vessel must qualify its own sector limits and cooling capacity during simultaneous responses.
Earth fusion uses the separate GENI Inverse Shield Mode.
Drone Integration · Revision 2
Four drone classes distributed between Fronak, Anorak and Zorak.
Design canon · Sources C1
- Allocated drones: 62
- Total berths: 74
- Reserve berths: 12
- Primary hosts: Fronak, Anorak, Zorak
Each research vessel has 4 Relay, 3 Deep-Space Survey/Inspection, 7 Planetary Survey and 2 Long-Duration Exploration drones. Zorak carries 8, 6, 14 and 2 respectively.
This R2 working allocation supersedes the earlier July table, which omitted the six Long-Duration drones. “Operational drones” is a design inventory term here; this hub does not report live availability.
Navigation & AGCM
Route verification, docking geometry and coordinated motion planning.
Concept · Sources S4, C1
- AGCM role: Geometry and route verification
- Associated systems: NEXUS, CMC, Atlas
AGCM verifies geometry, coordinate history and route legitimacy before acceleration, docking or high-risk field maneuvers.
Route uncertainty, thermal limits and reference disagreement remain reasons for hold or abort. No travel-speed claim is imported into this study document.
Vessel Medical & Survival
Medical integration, backup capacity and life-support coordination for the fleet.
Research scope · Sources C1
- Frameworks: ZSBIA-R1 · IMSI · MSO
- Backup references: ZHG-160R / ZHG-40R
- Research references: ZCEMT-R1 / ZCDTC-R1
The recorded program includes vessel backup ZHG-160R and distributed ZHG-40R, plus conceptual medical and treatment research.
Clinical performance, operational medical capacity and certification are not established by these project labels. Life support must retain its own qualified safety case.
Space Infrared Integration
Thermal inspection, docking awareness, plume diagnosis and scientific observation.
Integrated concept · Sources C1
- Coverage: Vessels, Atlas and survey drones
- Role: Sensing and diagnosis
The September integration spans hull and thermal-loop diagnostics, onboard fire detection, docking support, plume observation, astronomy and survey spectroscopy.
Detector selection, calibration, field of view and environmental qualification remain platform-specific work.
Frequency Travel
The Qi Fleet’s Frequency Travel hypothesis proposes following a current in space by tuning its GENI shields to the current’s measured signature.
Research hypothesis · Sources C1
- Control mode: Valley Lock
- Shield settings: Frequency and phase
- Capture signal: Velocity approaching the measured flow
Measure the current’s direction and velocity relative to the fleet. Sample its field signature along the planned route.
GENI adjusts the shield’s frequency and phase to couple to the current. AXIOM checks for a stable lock within the permitted operating limits.
Independent tracking checks whether the ships’ velocities converge with the flow. GENI tracks the changing field while NEXUS coordinates formation spacing.
Hold Jetnok’s stern thrust steady and alternate between a matched shield setting and a nearby detuned setting. Use independent tracking to look for repeatable acceleration along the current.
Zorak, three carriers and two research vessels travel as a formation in this concept. The eight interceptors ride docked. The stern drives and hull thrusters handle local manoeuvres.
IT-Jump Research
A separately tracked long-term research project within the Space branch.
Speculative concept · Sources C1
- Program reference: IT-Jump Project
- Readiness: No physical validation established
IT-Jump is retained as a research topic. A detailed controlled specification was not loaded, and no demonstrated travel capability is claimed.
Atlas & Scientific Observation
Observation and anomaly identification feeding the fleet research workflow.
Concept · Sources S4, C1
- Interfaces: NEXUS, AGCM, research vessels
- Anomaly doctrine: Atlas-triggered Group C response
Atlas supports observation and route records. Under the recorded Group C doctrine, Sorko stays near Zorak with Serko and Zotno docked.
Araknok and Ferko join anomaly missions automatically under the concept unless needed for flagship defense. Mission authorization and safety constraints remain separate from this study interface.
AXIOM
Enforces the permitted envelope and can demand a safe hold.
Framework · Sources S2, S4, S5
- Role: Final safety constraint
- Boundary: Cannot block autonomous protection
AXIOM applies safety constraints to permitted operation. In the Earth qualification baseline, it may impose a more conservative hold or shutdown, but may not block an autonomous magnet-protection trip.
The July document also describes AXIOM as governing laws and objectives. These study pages preserve that conceptual role while using the later Earth safety boundary where it applies.
NEXUS
Turns telemetry and models into diagnosis, prediction and coordination.
Framework · Sources S1, S2, S4
- Role: Supervisory digital twin
- Safety authority: No independent trip veto
NEXUS supports understanding, trend analysis and recommended action. It does not replace independent local protection or the ZENIT Safety Authority.
For Earth fusion it cannot alter trip thresholds, suppress protection, erase validated records or reconcile away an unexplained inventory discrepancy.
SERAT
Routes protected energy, manages heat and coordinates recovery.
Framework · Sources S1, S2, S4, S5
- Role: Energy and thermal management
- Boundary: Separate from primary energy generation
SERAT manages distribution, thermal loops, cooling, recovery and safe energy discharge. GENI manages field interaction; neither replaces the other.
Earth fusion retains a separate SERAT Energy Island. Space uses protected power corridors and separate distribution trunks under the vessel architecture.
GENI-10 / GENI
Coordinates field interaction and authorized energetic interfaces.
Concept · Sources S1, S2, C1
- Current naming: GENI-10
- Earth / Space: Use scoped shield modes
GENI controls field interaction, phase matching and energetic interfaces in the conceptual framework. It is not evidence of proven gravity control, propulsion or shielding.
Earth fusion uses GENI Inverse Shield Mode with five conceptual layers. Outverse is the Space mode and is not transferred into the Earth facility.
ZENIT Safety Authority
Owns independent acceptance, hazard closure and configuration control.
Governance · Sources S2, C1
- Abbreviation: ZSA
- Independence: From command, NEXUS and plant systems
ZSA owns the hazard log, approved test procedures, deviations, anomaly closure and final acceptance decisions.
Qualification requires evidence tied to the exact hardware, software and settings. A simulation result alone does not close a physical qualification gate.
Infrared sensing · ZIR-R1
Adds thermal imaging, diagnostics, navigation support and scientific observation.
Integrated concept · Sources C1
- Scope: Earth and Space
- Role: Sensing and diagnosis
The September integration covers condition monitoring, fire and hotspot detection, low-light awareness, thermal-loop and engine diagnostics, remote inspection, obstacle sensing and scientific infrared spectroscopy where appropriate.
Sensor data feeds processing and NEXUS diagnosis. SERAT and GENI responses remain within AXIOM constraints and independent safety governance. Infrared sensing is not a substitute for qualified safety protection.
Fusion A / B
Separate primary-energy lanes, each with its own protected interface.
Concept · Sources S1, C1
- Boundary: Power generation, separate from CMC
Each core feeds its Local Fuse Chamber. Reactor safety paths must remain locally independent.
Local Fuse A / B
Isolates and conditions the output of each source.
Concept · Sources S1, C1
- Rule: One protected interface per core
The Local Fuse Chamber contains faults at its source before power is coordinated centrally.
Central Bidirectional Fuse
Coordinates the protected A and B source lanes.
Concept · Sources S1, C1
- Current working arrangement: Two protected lanes
The central chamber coordinates source selection, balancing, bidirectional transfer and isolation. Independence must be demonstrated rather than assumed.
Vector Accelerator
Uses conditioned and authorized power in the conceptual propulsion chain.
Speculative concept · Sources S1, S4, C1
- Input: SERAT power / GENI control / CMC reference
The Vector Accelerator is a conceptual conversion and command-conditioning stage. This reference provides no demonstrated thrust, speed or propulsion efficiency.
Central Magnetic Core
Supplies the vessel magnetic reference, synchronization and compensation.
Concept · Sources S1, S4, C1
- Boundary: Separate from fusion core
CMC compares reference anchors and supports an accepted vessel reference. It neither generates primary power nor provides proof of propulsion.
Independent Reactor Safe Island
Provides a local reactor path to terminate, dump energy, cool and isolate.
Concept · Sources S1
- Abbreviation: IRSI
- Independence: From NEXUS and the opposite reactor
The conceptual island includes hardwired termination, field-energy discharge, quench protection, protected power, cooling and mechanical isolation.
AGCM
Checks geometry, route legitimacy and coordinate history.
Concept · Sources S4
- Interfaces: NEXUS / CMC / navigation
AGCM supports route and docking checks. It does not justify motion through uncertain geometry.
Gravity Control Chambers
A speculative internal acceleration-frame management concept.
Speculative concept · Sources S4, C1
- Validation: Not established
GCC belongs to the long-term conceptual architecture. Proven gravity control is not claimed.
Source references
S1 · Core Architecture · Single File · Space energy chain; CMC, GENI, IRSI, fuse chambers, SERAT and Vector Accelerator. Conceptual educational reference. Original reference
S2 · Fusion Qualification · WP3 R1 · ZFPQ-WP3-R1. Authoritative for the Earth quench and tritium qualification work packages. Definition complete; physical execution open. Original reference
S3 · Critical Capability Register · R1 · ZFCCR-R1. 32 planning risks and 10 decision gates; supplier and test-capacity candidates. No confirmed procurement or test booking. Original reference
S4 · Canonical Engineering Baseline · v1 · Earlier conceptual framework: subsystem separation, fleet roles, AGCM and operating principles. Later scoped revisions take precedence. Original reference
S5 · Core Principles · Selected Slides · Purpose and common principles: Earth energy, mobility, SafeSpots, LSI, environmental responsibility; Space exploration and survivability. Older mobility diagrams are not the current drivetrain baseline. Original reference
S6 · Aurora Shield · 15-Region Outverse Design · Five functions in each of three main layers, with individual pass checks and Zorak’s single-sector simulation results. Original reference
C1 · ZENIT working project context · Working project context includes mobility specifications, the 24 July fleet flight design, fleet docking doctrine, Frequency Travel research, Drone Integration R2, QVCO-R1, recorded model exercises, medical projects and infrared integration. The underlying specification files were not loaded for these entries.
Contact ZENIT
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Drone models
Chronicles — Optem mission summaries
Zorak flagship model
Weapons impact log
Outverse Shield overview