Services — Aexion Synthesis

Data Acquisition & Telemetry

DAQ

High-frequency multi-channel telemetry capture across all critical engine parameters — thrust, chamber pressure, propellant temperatures, and mass flow rates. Synchronized multi-camera video recording enables frame-accurate event correlation. Raw data is archived in traceable format with full calibration metadata.

Thrust (dual sensor)
Chamber pressure (Pc)
Propellant temperatures
LOX & IPA mass flow
Valve state channels
Multi-camera sync video

L1 Descriptive Analytics

Report

Comprehensive time-series analysis across 15+ parameter channels. Interactive HTML reports include statistical summaries, KPI dashboards, per-channel charts with outlier detection, and embedded video playback. Atmospheric conditions are applied automatically using climatological corrections for the test site elevation.

15+ parameter tabs
Statistical summaries
Outlier detection (IQR)
Embedded video player
Atmospheric corrections
Self-contained HTML

L2 Diagnostic Analytics

Diagnostic

Deep-dive combustion quality assessment with derived performance parameters. Computes characteristic exhaust velocity (c*), thrust coefficient (CF), specific impulse (Isp), and oxidizer-to-fuel ratio (O/F) from measured data. Ignition event classification, transient analysis, and combustion stability metrics provide actionable insight for engine development teams.

c*, CF, Isp, O/F
Ignition classification
Combustion stability
Transient analysis
Anomaly flagging
JANNAF parameter set

Campaign Comparative Analysis

Campaign

Multi-test campaign overview and cross-test comparison in a unified dashboard. The Campaign HUB aggregates key metrics across all tests for trend identification and program-level visibility. The COMP Comparative report overlays performance parameters side-by-side, supporting regression and improvement tracking across engine development iterations.

Campaign HUB dashboard
COMP side-by-side view
Trend identification
Cross-test KPI table
Program-level summary

Standards Compliance

JANNAF

Structured documentation aligned with JANNAF GL-2012-01 reporting methodology. Deliverable packages include both interactive HTML analytics and formatted Word document reports. All data references are traceable, atmospheric corrections are documented, and parameter definitions follow JANNAF conventions — supporting program review and export-controlled deliverables.

JANNAF GL-2012-01 referenced
HTML + DOCX deliverables
Traceable data chain
Calibration records
Parameter glossary

Why Aexion

Built for Propulsion
Development Programs

Our platform is purpose-built for the realities of liquid rocket engine testing — not adapted from generic data tools.

// OFFLINE FIRST

No Server Required

All analytics outputs are self-contained HTML files. Open them locally, share via email, or host on any server. No cloud dependency, no recurring infrastructure cost, no data exposure risk.

// AUTOMATED PIPELINE

Minutes, Not Days

From raw CSV telemetry to a complete diagnostic report in minutes. The automated pipeline eliminates manual post-processing, letting your team focus on engineering decisions — not data preparation.

// DOMAIN SPECIFIC

LRE-Native Parameters

Every metric, chart, and report structure is designed around liquid rocket engine testing. JANNAF parameter definitions, nozzle geometry constants, and combustion stability metrics are first-class citizens — not afterthoughts.

// PROVEN IN FIELD

Field-Validated

The platform has been validated in production hot fire tests with a LOX/IPA engine at the Thrust.kz test facility, delivering measured thrust, chamber pressure, and O/F data — with complete L1/L2/HUB/COMP report packages.

What We Deliver