Aerospace Intelligence

More than a Software,

Design, Build and Verify with Confidence.

Explore more ↓

LOCAL-FIRST · CLOUD ACCESS OPTION AVAILABLE

Built for sensitive aerospace environments

AETHER runs locally, inside the customer network, air-gapped, or on approved cloud servers. Use AETHER models, local backends, or customer-approved internal model servers. Controlled data uploaded to our cloud servers is governed by a strict policy.

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