RAI-ROCKET-001 / Completed simulation study
Payload_Rocket_V1
RAI / Evidence-led development
An OpenRocket conceptual engineering study. Every performance value below is a model output, not a measured flight result.
Engineering objective
Explore stability and mission trade-offs in simulation.
The work used OpenRocket to evaluate a conceptual rocket configuration, motor selection, predicted apogee, modeled mass and static stability.
Simulation evidence
- Predicted apogee: 312 m
- Modeled stability: 2.4 calibres
- Modeled mass: 840 g
- Motor represented in model: G74W-9
Validation state
OpenRocket modelCompleted
Physical buildNot evidenced
Ground testNot performed
Flight testNot performed
Declared limitation
Simulation is not flight evidence.
Outputs depend on geometry, mass, aerodynamic assumptions, motor data and environmental inputs. Physical work would require verified design, legal and range approval, inspection, recovery testing and qualified supervision.