Aerospace Intelligence

More than a Software,

Design, Build and Verify with Confidence.

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LOCAL-FIRST · CLOUD ACCESS OPTION AVAILABLE

Built for sensitive aerospace environments

AETHER RUNS LOCALLY, INSIDE THE CUSTOMER NETWORK, AIR-GAPPED, OR IN AN APPROVED CLOUD SERVERS. USE AETHER MODELS, LOCAL BACKENDS, OR CUSTOMER-APPROVED INTERNAL MODEL SERVERS. WE HAVE A STRICT POLICY AROUND CONTROLLED DATA UPLOADED IN OUR CLOUD SERVERS.

AETHER LOCAL

Runs on the engineer's machine

Local project vault, local math brain, local model runtime, and no outbound telemetry by default.

CLIENT EDITION

Customer-bound and versioned

Signed builds labelled like local-run-AETHER-client-version, with customer-specific deployment manifests.

ON-PREM / AIR-GAP

Inside controlled networks

Company-hosted models, document indexes, RBAC, audit logs, and offline-capable deployment for restricted programmes.

AETHER CLOUD

For non-sensitive work

Cloud access remains available for demos, education, public data, and customer-approved low-risk workflows.

BUILT FOR

  • AEROSPACE COMPANIES
  • START-UPS
  • DRONE / eVTOL
  • DEFENSE & MILITARY
  • INDEPENDENT ENGINEERS
  • ACADEMIC INSTITUTIONS

FIVE ENGINES · NO PIPELINE

Independent by design

Each engine operates independently, addressing its own class of analysis. Engage one or all five; no engine depends on another's output, and no fixed sequence is imposed.

(01)ARITHMOSCompute

Analytical and numerical solutions, fully derived

Aero, thermal, structures, orbital, propulsion and control — assumptions and validity shown.

OPEN ENGINE →

(02)MORPHDesign & Code

From system design to flight-grade code

Verified Ada/SPARK, C/C++, MATLAB/Simulink and Python — structured for review and test.

OPEN ENGINE →

(03)TELOSRequirements

Requirements engineered for full traceability

Drafts, traces and checks requirements, then converts them into test cases.

OPEN ENGINE →

(04)THEMISCompliance

Artifacts assessed against the governing standards

DO-178C, DO-254, AS9100, ARP4754A/4761, FAA/EASA and ITAR — checked clause by clause.

OPEN ENGINE →

(05)DYNAMISAvionics & Embedded

Avionics architecture, end to end

Interface control, power and signal budgets, hardware compliance and fault tolerance.

OPEN ENGINE →

THE GLASS BOX

Every result shows its derivation

A result that cannot be traced cannot be certified. Every engine returns the governing basis, the stated assumptions, the computed values, and the resulting artifact — in that order, without exception.

ARITHMOS · ORBITAL MECHANICS · HOHMANN TRANSFER

EQUATION Δv₁ = √(μ/r₁) · ( √( 2r₂ / (r₁+r₂) ) − 1 )

ASSUME two-body · impulsive burns · coplanar circular orbits

INPUT r₁ = 6 778 km (LEO 400 km) → r₂ = 42 164 km (GEO)

DERIVE aₜ = ½(r₁+r₂) = 24 471 km · v₁ = 7.669 km/s

RESULT Δv₁ = 2.397 · Δv₂ = 1.457 · Δv_total = 3.854 km/s

--  SPARK: provable, no runtime errors
function Hohmann_Total_Dv (R1, R2 : Orbit_Radius) return Delta_V
  with Pre  => R2 > R1,
       Post => Hohmann_Total_Dv'Result > 0.0;

VERIFIED · TRACEABLE TO FIRST PRINCIPLES

ACCESS & DEPLOYMENT

Choose the runtime that fits the data.

Cloud for non-sensitive work · Local and on-prem for controlled engineering environments

PRO

$29/mo

  • Single seat cloud access
  • Any two engines of your choice
  • Worked derivations on every result
  • For public or non-sensitive work
Start 3-day trial

RECOMMENDED

ULTRA

$199/mo

  • All five engines
  • Local desktop path for customer-controlled projects
  • Requirements trace & test-case export
  • Customer-selectable local model backends
Get Ultra access

ENTERPRISE / CONTRACT

Customannual

  • Multi-seat, all engines
  • On-prem, private VPC, or air-gap deployment
  • Customer-bound signed builds and audit logs
  • CUI / ITAR / EAR-aware deployment planning
  • Dedicated engineering and security liaison
Request enterprise pilot

AETHER · AEROSPACE INTELLIGENCE

Verifiable answers.
Customer-controlled deployment.

Start 3-day trial Request enterprise pilot