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QUANTRIX DEEPTECH STUDIO|FRONTIER R&D 2026

Architecting Systems Beyond The Horizon

Creating the next generation of products before they exist. We design and engineer mission-critical technologies across space, aerospace, defense, cybersecurity, and AI — turning undefined physical and computational problems into operational reality.

05Core Domains
TRL 7+Prototyping
0.00%Hallucination
DO-178CAudit Certified
ORBITAL RADAR // SCOPE
RANGE: 1200 KM
000° N180° S090° E270° W
TARGET_TELEMETRYLOCKED

RIGEL-ALPHA

Aerospace Physics Kernel
1420.405 MHzGEO 35,786 KM

Deterministic Shigley Derivation // Mach 4.2

SIGNAL STRENGTH:
AZIMUTH: 042°DIST: 816 KM
OpenCASCADE B-Rep KernelSolid Modeling
CalculiX Nonlinear FEAStructural Analysis
Gmsh Tet10 Adaptive MeshPre-Processing
DO-178C Level A AuditAerospace Standard
AS9100D Rev D QualityDefense Compliant
Local LLaMA 3.2 ParserDeterministic NLP
SHA-256 Cryptographic ChainZero Hallucination
Air-Gapped Local-FirstZero Cloud
Shigley 11th Ed. EquationsAnalytical Physics
OpenCASCADE B-Rep KernelSolid Modeling
CalculiX Nonlinear FEAStructural Analysis
Gmsh Tet10 Adaptive MeshPre-Processing
DO-178C Level A AuditAerospace Standard
AS9100D Rev D QualityDefense Compliant
Local LLaMA 3.2 ParserDeterministic NLP
SHA-256 Cryptographic ChainZero Hallucination
Air-Gapped Local-FirstZero Cloud
Shigley 11th Ed. EquationsAnalytical Physics
01 // ARCHITECTURAL DIVISIONS|PIN LOCKED • SCROLL TO ADVANCE

Deeptech Focus Areas

01 / 06
ALL SPECS
SYS-01|SECTOR 01
ACTIVE R&D

Space Systems

Operational Vector

Autonomous architectures for orbital, ground, and constellation operations with real-time perturbation compensation.

Constellation telemetry and mission-aware orbital planning.
TECHNICAL SUBSYSTEMS
Orbital OperationsSmallsat ArchitectureLEO/GEO Telemetry
EXPLORE SPECIFICATION
SYS-02|SECTOR 02
SIMULATION READY

Aerospace Engineering

Operational Vector

Guidance, navigation, and control algorithms operating at the thermodynamic and physical envelope of hypersonic flight.

Autonomous flight path vectoring and supersonic stress boundaries.
TECHNICAL SUBSYSTEMS
GNC AlgorithmsSupersonic DynamicsFlight Telemetry
EXPLORE SPECIFICATION
SYS-03|SECTOR 03
TACTICAL SPEC

Defense Technology

Operational Vector

High-reliability embedded avionics designed to withstand electronic warfare, kinetic disruption, and signal denial.

Tamper-proof hardware systems built for contested operational envelopes.
TECHNICAL SUBSYSTEMS
Hardened HardwareResilient CommsFail-Safe Protocol
EXPLORE SPECIFICATION
SYS-04|SECTOR 04
ZERO-TRUST

Cybersecurity

Operational Vector

Formally proven micro-kernels and hardware security modules ensuring absolute partition isolation.

Cryptographically isolated execution with zero external cloud vectors.
TECHNICAL SUBSYSTEMS
Cryptographic IsolationAir-Gap ArchitectureMemory Safety
EXPLORE SPECIFICATION
SYS-05|SECTOR 05
EDGE INFERENCE

Artificial Intelligence

Operational Vector

Physics-informed neural networks executing at sub-millisecond latency on edge avionics silicon.

Deterministic, zero-hallucination local models for critical guidance.
TECHNICAL SUBSYSTEMS
Real-Time Sensor FusionAutonomous TrajectoryNeural Guidance
EXPLORE SPECIFICATION
SYS-06|SECTOR 06
SYNTHESIS

Full-Stack Synthesis

Operational Vector

End-to-end integration synthesizing microcode, physical dynamics, and ground telemetry into unified missions.

Unified hardware-in-the-loop validation spanning multi-domain architectures.
TECHNICAL SUBSYSTEMS
Cross-Domain BusHardware-in-LoopE2E Telemetry
EXPLORE SPECIFICATION
01
06
Vertical wheel scrubs horizontally (01/06) • Complete all 6 divisions to reach Section 3
02 // FLAGSHIP INITIATIVE

Project Rigel

Deterministic engineering infrastructure for aerospace where physics equations derive geometry directly.

STAGE 1 // MVP IN ACTIVE FLIGHT VALIDATION

Deterministic CAD & FEA: Physics Derives Geometry

Deterministic engineering infrastructure for aerospace where physics equations derive geometry directly. One plain-English sentence becomes a STEP file, FEA report, and SHA-256 audited engineering package. No CAD. No hallucination. No cloud.

Analytical Physics Kernel deriving dimensions directly from Shigley equations
Local LLaMA 3.2 NLP parser (null on uncertainty, zero hallucinations)
Automated Gmsh Tet10 meshing & CalculiX FEA with < 5% mesh convergence
SHA-256 cryptographic audit chain engineered for DO-178C & AS9100
Open Rigel WorkspaceRIGEL.QUANTRIX.STUDIO
RIGEL // PHYSICS WORKBENCHDeterministic Dimensional Derivation
SHIGLEY EQ 6-2: BENDING THICKNESSAL 6061-T6 // FOS 2.5
t=
6 × 200,000N·mm40 mm × 110.4 MPa
=16.48 mm
Direct closed-form derivationσ_max = 110.4 MPa
DYNAMIC CROSS-SECTIONFEA GRADIENT
b=40mm | t=16.48mm
Tension (Top) Compression (Bottom)
4000 N
1 kN (Light Test)10 kN (High G-Force)
50 mm
10 mm (Flush Bracket)100 mm (Extended Cantilever)
40 mm
20 mm (Narrow)80 mm (Wide Flange)
2.5x
1.5 (Aero Margin)4.0 (Mission Critical)
DERIVED THICKNESS (t)16.48 mm
σ ALLOWABLE110.4 MPa
ESTIMATED Δ DEFLECTION0.16 mm
SHA-256 AUDIT: 7f4c9a81e3d09a2b54...LOCAL-FIRST // ZERO CLOUD DEPENDENCY
03 // AUTONOMOUS ARCHITECTURE

Deterministic Pipeline Flow

From plain-English requirement to verified solid CAD model in under 4 seconds with zero hallucinations.

STAGE 01 // DEEP INSPECTION| 420 ms EXECUTION

Spec Ingestion: Plain-English Engineering Prompt

Engine Core:LLaMA 3.2 3B (Local Ollama)
INPUT CONSTRAINT / PAYLOAD

"Design an aerospace L-bracket for 4000N axial load with 50mm moment arm in Al 6061-T6 with 2.5 FOS."

SYNTHESIZED DETERMINISTIC ARTIFACT

JSON Parameter Map: { load: 4000, arm: 50, material: 'Al-6061-T6', fos: 2.5 }

Deterministic Parser: Returns NULL on ambiguous syntax. Zero hallucination guarantee.

EXECUTION_KERNEL_TRACE
STAGE_01_OK
// Raw Input: Natural language constraints
const inputSpec = {
  load_axial_N: 4000,
  moment_arm_mm: 50,
  material_spec: "AMS 4027 (Al 6061-T6)",
  yield_strength_MPa: 276,
  required_FOS: 2.5
};
Total Pipeline Latency: <3.8 secondsDeterministic Guarantee: 100%
04 // OPERATING DOCTRINE

Engineering Axioms

The non-negotiable principles guiding every architecture, prototype, and product system we build.

[01]RAPID ITERATION

Asymmetric Velocity

We compress complex aerospace development lifecycles by executing rapid physical and software prototypes rather than remaining trapped in bureaucratic review cycles.

DOCTRINE VERIFIED
[02]PHYSICS FIRST

Empirical Validation

Simulations provide mathematical intuition; real-world telemetry and boundary stress tests decide empirical truth. We validate at the envelope's edge.

DOCTRINE VERIFIED
[03]ZERO COMPROMISE

Full-Spectrum Resilience

In critical aerospace and defense systems, failure is intolerable. From micro-firmware to distributed ground layers, security and fault tolerance are foundational.

DOCTRINE VERIFIED
[04]DEEPTECH RADICAL

Frontier-First Mandate

We intentionally target high-consequence, undefined problems where off-the-shelf commercial software and CAD fail to meet physical and computational demands.

DOCTRINE VERIFIED
05 // ENTERPRISE ASSURANCE

Technical Assurance

Addressing deeptech, defense procurement, air-gapped security, and certification requirements.

Generative CAD plugins use probabilistic neural networks that hallucinate polygon meshes without physical constraints, resulting in non-manufacturable geometries. In contrast, Rigel is an analytical physics engine. It uses local LLM strictly for parsing natural-language constraints into formal parameter sets, and then executes deterministic closed-form mechanical engineering formulas (e.g. Shigley, Roark) to compute geometry directly. 100% reproducible, zero hallucinations.