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SPACE LOGISTIX / Launch and cargo vehicles / CONCEPT

Geometry begins the qualification process.

Usable envelopes, adapters, allowable loads and ICD documentation must be assessed together. The external fairing diameter is not the approved payload space.

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ENGINEERING STUDY

Falcon 9

Concept integration configuration. Requires engineering verification and approval by the mission operator.

  • Approved static and dynamic envelopes
  • Adapter, clearances and fixture access
  • Mass, centre of gravity, vibration and loads
  • Separate fairing transport from hatch access

No container count or compatibility approval is specified. Pressurized vehicles additionally require hatch dimensions, crew requirements and material safety assessment.

Manufacturer references

Falcon 9 / Falcon Heavy — Falcon User’s Guide

Ariane 6 — manufacturer documentation

Vega-C — Avio User’s Manual, Issue 1 Rev 0 / September 2025

Sources reviewed: 9 October 2026. The applicable documentation revision must be agreed for each mission.

Manifest data overview

Existing manifest database integration. DEMO data does not confirm slots or partnerships. No booking or container qualification is performed.

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Concept in development. Parameters, interfaces and applications require documentation, testing and mission-specific approval.

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