1 – Scaled erection/retraction system
Name of the system:
Scaled erection/retraction system
Lead entity within the SAMMBA consortium:
MT Aerospace
Attachment point within the process chain of the Spaceport operator:
The system responsible for erecting and retracting the microlauncher at the launch pad.
Major benefit [KPI] within the process chain: [cost reduction/processing time reduction/reliability
increase – preferably with quantitative figures]
Increase in compatibility with multiple launchers: The erection/retraction system is not dedicated to a specific launcher but is comptabile with multiple launchers.
Anticipated R&D vector for the near/mid/long-term:
Near-term targeted market segment: operational for one mini-launcher
Mid-term targeted market segment: operational for several mini-launcher
Long-term targeted market segment: bigger launcher
Modularity granted with the following standards:
The scaled erection/retraction system doesn’t require special modifications and can be used at any spaceport.
Interoperability granted with the following standards:
Fixation of the system on the ground/surface to avoid moving during launch
Systems interfaced:
Launcher, AGV for transport of the launcher, mechanical structures
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