Group 1 · Engineering
Rocket body height
| Nose section | 8 000 | mm |
| Payload bay | 1 200 | cm |
| Engine section | 0.025 | km |
↑ add the three numbers above
↑ convert each to m, then add
Total =
m
Group 2 · Engineering
Engine bell diameter
| Inner nozzle | 500 | mm |
| Middle ring | 20 | cm |
| Outer flange | 100 | mm |
↑ add the three numbers above
↑ convert each to m, then add
Total =
m
Group 3 · Mission Control
Launch pad clearance
| Support base | 1 000 | cm |
| Main frame | 0.03 | km |
| Safety buffer | 10 000 | mm |
↑ add the three numbers above
↑ convert each to m, then add
Total =
m
Group 4 · Mission Control
Antenna total height
| Base mount | 150 | cm |
| Main mast | 1 200 | mm |
| Tip element | 30 | cm |
↑ add the three numbers above
↑ convert each to m, then add
Total =
m