This is a second iteration of the Pir-hana design, the F5000. There are several design flaws that this revision aims to target, these are outlined by the following requirements:

• Field access to anchors and recovery system without tooling.
• Airframe material with more options for hardware mounting methods, and better graphics.
• Multiple seperate bays, options for dual-deploy while maintaining sufficient avionics.
• Options for multiple weight mount points, expanding range of applicable motor classes, while maintaining single-deploy recovery and sufficient stability.
• Mount point for forward fin group, expanding range of applicable motor classes without significantly reducing apogee.
• Reproducibility, full CAD and laser models for both manufacturing and assembly.

• To be completed.