Production Analytics Platform  ·  LRE Testing

Precision Analytics
for Rocket Propulsion
Testing

Aexion Synthesis delivers advanced data acquisition and diagnostic analytics for liquid rocket engine development. From raw telemetry to structured, JANNAF-referenced reports — in one platform.

LOX / IPA System Thrust.kz Test Stand JANNAF-Referenced Reporting Almaty, Kazakhstan
Report Types
4
L1 · L2 · HUB · COMP
Peak Thrust
413 kgf
4.05 kN · LOX/IPA
Burn Duration
13.27 s
Full burn window · sustained
Chamber Pressure
1.43 MPa
Avg Pc · measured · LOX/IPA
End-to-End Propulsion
Testing Analytics

From sensor setup and data capture to diagnostic reports and campaign-level analysis — Aexion handles the full data stack.

DAQ
Data Acquisition

Multi-channel high-frequency telemetry capture across thrust, chamber pressure, temperatures, and propellant mass flow — with synchronized multi-camera video recording.

L1·L2
Analytics Platform

Automated L1 descriptive and L2 diagnostic reports with interactive dashboards, time-series visualizations, performance metrics, and combustion quality assessment.

RPT
Compliance Reporting

JANNAF GL-2012-01 referenced documentation packages with traceable data chains, atmospheric corrections, and structured deliverables ready for program review.

From Raw Telemetry
to Diagnostic Report

Automated pipeline from DAQ output to publication-ready analytics — no manual post-processing required.

  • L1 Descriptive analytics · 15+ parameter channels
  • L2 Diagnostic deep-dive · combustion quality metrics
  • Campaign HUB · multi-test comparison view
  • Atmospheric corrections applied automatically
  • Inline synchronized video playback
  • Self-contained HTML output · no server required
Explore the Platform →
LRE_L1_Descriptive.html
Overview
Thrust
Pressure
Temperature
Performance
Video
Peak Thrust
413
kgf
Burn Duration
13.27
seconds
Avg Pc
1.432
MPa
O/F Ratio
1.41
measured
Thrust Force · Full Burn Window
3s 6s 9s 12s 450 225 0 kgf
Ready to Advance Your
Propulsion Program?

Our platform supports every phase of liquid rocket engine development — from first ignition to campaign-level comparative analysis.

Get in Touch →