Live planner

Structure print planner

Estimate mass saved, material required, print duration, and mission risk before committing to a structure. Outputs sync to your construction dashboard.

Open dashboard

Space structure print planner

Configure arrival-side construction

Compare what you launch against what you can print after arrival — before design lock.

Structure type

Mission locationMaterial sourceStructure sizeLoad requirementPrint methodMission urgencyLaunch constraint

Stores to your mission dashboard for traceability.

Orbital print envelope

Material demand: 126 kg
Print duration: 30 h
Launch mass saved: 65%
Structural complexity: 90/100
Risk posture: Low — feasibility 96/100

Construction mission

Habitat frame · LEO

Hybrid launched + ISRU · Continuous fiber extrusion · Balanced program

Print feasibility

Net print mass demand

126 kg

Scaled against a reference 800 kg orbital print campaign.

Launch mass saved

65%

vs. monolithic launch assembly — includes avoided fairing volume 0.7 m³

Print duration

30 h

Wall-clock estimate for qualified print cell.

Structural risk

Low

Complexity index 90/100 (derived).

Print duration

30 h

1. Survey & anchor grid4h

2. Feedstock staging5h

3. Primary print pass14h

4. Integration & stiffening5h

5. Verification release2h

Print method recommendation

Continuous fiber extrusion

Compared to selected: Continuous fiber extrusion

Launch constraint comparison

Active profile Balanced program — drives fairing volume credit and schedule buffers in the feasibility model.

Construction risk matrix

Overall: Low

structural

Low

thermal

Low

logistics

Low

schedule

Low