| Project purpose |
Level 2 certification |
|
| Airframe diameter |
54 mm (approximately 2.1 in) |
|
| Airframe configuration |
Minimum diameter |
Motor-to-airframe configuration |
| Main body tube |
Wildman Rocketry G12-2.1 fiberglass tube, 34.157 in long |
ID 2.152 in; OD 2.276 in |
| Development status |
In development |
|
| Motor |
AeroTech L1000W DMS |
Purchase status unconfirmed |
| Predicted apogee |
Approximately 20,000 ft |
Simulation prediction |
| Predicted maximum Mach |
Approximately Mach 2.2 |
Simulation prediction |
| Nose cone |
54 mm Von Karman |
|
| Fin material |
FR4 / G10 |
|
| Fin count |
3 |
|
| Fin root chord |
6.6676 in |
|
| Fin span |
2.3134 in |
|
| Fin tip chord |
2.6798 in |
|
| Fin sweep distance |
3.6950 in |
|
| Fin thickness |
0.1867 in |
|
| Fin distance from tube base |
7.6099 in |
|
| Fin airfoil section |
Double Wedge |
|
| L.E. diamond airfoil length |
0.2500 in |
|
| Fin leading-edge radius |
0.0000 in |
|
| Recovery architecture |
Dual deployment, head-end configuration |
|
| Main parachute |
Fruity Chutes Iris Ultra Compact, 36 in |
|
| Avionics coupler tubes |
Wildman Rocketry G12CT-2.1, 6 in long |
ID 2 in; OD 2.15 in; dual-deployment unit |
| Switch band |
54 mm, 1 in wide |
|
| Flight computer |
Missile Works RRC3+ |
|
| GPS tracker |
Featherweight Swift |
|
| Ground station |
Featherweight ground station |
|
| Camera |
RunCam Split 4 V3 |
|