Exhibit 02 of 03Built & Validated

Ostia

The modular static-fire stand that holds the motor, takes its thrust, and records the burn.

Status
Built & Validated
Medium
SolidWorks · Ansys Workbench · DAQ
Role
President & Propulsion Lead — NEAL Aerospace

Everything NEAL builds ends up bolted down and fired horizontally. Ostia is the infrastructure for that: a modular welded-steel stand that holds Remus on a linear rail, takes its thrust through a pair of load cells into a gusseted wall, and records the burn.

Simulated static fire of Remus on the Ostia stand at sunset, plume exiting to the left
Remus firing on Ostia — simulated plume, not test footage

I designed the structure in SolidWorks for 1,000 lbf of thrust at a 2.5 factor of safety and analysed it in Ansys. The thrust wall and gussets pass with room to spare. The load-cell flexures and the 1/4 in base plate fall short of 2.5, so the load-cell mounting and the rocket clamp are being redesigned; the results shown are for the stand as drawn.

Close-up of the load cell mounted behind the thrust plate on the Ostia stand
2,000 lbf load cell on the thrust axis, logged at 1 kHz

The stand carries a 2,000 lbf load cell on the thrust axis and thermocouples on the chamber, logged at 1 kHz. That is fast enough to capture the ignition transient and the shape of the thrust curve, which is what closes the loop back to the injector models.

Remus on Ostia

The full stand

Motor, clamp, linear carriage, thrust plate and load cells on one base plate. Thirty-six pre-rendered frames, scrubbed by scroll.

Ostia analysis

8 frames

Ostia renders

8 frames