Where P1 fits
Aerospace, Defense, and Space programs face different constraints. P1 works from each program's constraint set, including loads, materials, thermal range, and mass.
Airframe structural design
Airframe structures often require repeated FEA setup as designs change. P1 takes material, load, boundary, thermal, and mass inputs and returns design candidates for review, so each iteration starts with options rather than a blank page.
- Airframe brackets for multi-axis load conditions
- Fuselage mounts with structural and thermal limits
- Floor and bulkhead layouts within mass limits
- Secondary airframe structures within mass limits
Defense propulsion and thermal structures
Defense propulsion mounts and thermal structures combine load, shock, vibration, and thermal constraints. P1 generates candidate geometries from these inputs, giving teams a shared set to review instead of handling each constraint separately.
- Enclosures for shock and vibration loads
- Mounts across a wide thermal range
- Structures within volume and mass limits
- Candidates for specification revisions
Satellite and propulsion structures
Satellite bus frames and propulsion structures must fit material, load, boundary, thermal, and mass requirements. P1 generates candidates from the combined constraint set, so engineers can review linked requirements rather than vary one axis at a time.
- Satellite panel and bus frame topology
- Propulsion mounts and bracket structures
- Attitude hardware with tight mass limits
- Thermal and structural orbit-ready geometries
P1 works from your constraints
Set your program constraints. Review the candidates P1 generates.