Concept RenderBooster-assisted launch
Boosters fitted, sized to the hexagonal guide rails that set the 36-cell packing.
- Launch diameter30" (762 mm)
- Launch weight1,614 lb (734 kg)

Bee-MX is a hexagonal-section missile designed from the container inward. The same six facets that let the airframe tessellate inside an ISO magazine serve as its guide rails on launch, so magazine depth stops being a function of bespoke cells and becomes a function of floor area.
Forty seconds: shipping container, emplacement, salvo, cruise.
Animated concept sequence. Not test footage, and not a depiction of qualified hardware or demonstrated performance.
Bee-MX carries a hexagonal cross section. The six facets let units nest in a close-packed array and index on hexagonal guide rails at launch. A boosted state is sized to those rails; a ramjet state flies the mission.
Concept RenderBoosters fitted, sized to the hexagonal guide rails that set the 36-cell packing.
Concept RenderBoosters spent. Ramjet nacelles arranged around a hexagonal airframe, with the shared central fuel tube running the length of the body.
Concept renders. Full engineering specifications and test plans are available under NDA to qualified government and prime-contractor partners.
Bee-MX leaves the magazine on its own rails, accelerates on three boosters, and then cruises on ramjet power at Mach 3. Nothing in the sequence requires a dedicated launch pad, crew emplacement, or site preparation.
The unit leaves the container on its hexagonal guide rails. No dedicated launch pad, crew emplacement, or site preparation.
Three boosters carry the airframe off the guide rails and up to ramjet operating speed.
Three ramjet engines sustain Mach 3 cruise, fed from the shared central fuel tube that runs the length of the body.
Autonomous guidance with integrated thrust vectoring carries the unit through the end of its flight.







Boosters fire together and carry the unit off the container's guide rails.
Thirty-six units ride in one unmodified 40-ft ISO container: three rows of 12, hexagonal close-packed with a 50% row offset. The hexagonal guide rails that launch each unit also set the packing.

Three ramjet engines and three boosters, carried on guide rails around a hexagonal airframe and fed by one shared central fuel tube. A parts-minimized design keeps control complexity low and the packing envelope clean.

A single central fuel tube runs the length of the body, with three ramjet engines on guide rails around it.

Three boosters with guide rails ride the hexagonal launch geometry out of the container. The launch configuration also carries integrated thrust vectoring.
Load, move, emplace, deploy. Every step uses equipment and routes that already exist.
01LoadLoaded with standard handling equipment.
02MoveTruck, rail or sea. No purpose-built carrier.
03EmplaceAn unmodified 40-ft ISO container. No site prep.
04DeployRack extends: 36 cells, hex close-packed.
Ships, arms and launches from an unmodified standard container.
A full container mobilizes and fires in under a minute.
Unit cost target at volume.

Every leg of the journey already exists. Bee-MX travels inside an unmodified 40-ft ISO container, so the equipment that moves it is the equipment already moving everything else.
SeaLeg
YardStagedIllustrative of the existing intermodal logistics network. Concept renders, not photographs of fielded equipment.

Bee-MX travels in an unmodified 40-ft ISO container, on the same truck, rail and sea network that already moves global cargo. Transport only gets it there. Once emplaced, it needs no dedicated launch pad and no site preparation.
Bee-MX is in Phase I, preliminary studies, with patents pending in the U.S. and abroad. Cretus Innovations is developing Bee-MX independently and is actively seeking government procurement opportunities, strategic partnerships, and prime-contractor relationships. The path from here runs through ground testing, flight testing and qualification toward fielding.
Steps 03 to 07 describe the intended development path. Timing depends on funding and partner engagement.

Geometry, packing density, propulsion arrangement and program schedule are released to government, prime and investor parties under NDA. Tell us which of those you need and we will scope the session.