Terran R
Terran R is a heavy-lift two-stage, partially reusable launch vehicle under development by Relativity Space. The vehicle is partially constructed with 3D printing technologies, much like its predecessor, the small-lift Terran 1. The first flight is expected to be in 2026.
| Manufacturer | Relativity Space |
|---|---|
| Country of origin | United States |
| Size | |
| Height | 82 m (270 ft) |
| Diameter | 5.5 m (18 ft) |
| Stages | 2 |
| Capacity | |
| Payload to LEO | |
| Mass | ~33,500 kg (73,900 lb) |
| Launch history | |
| Status | Planned |
| Launch sites | Cape Canaveral LC-16 |
| First flight | NET 2026 |
| First stage | |
| Powered by | 13 Aeon R |
| Maximum thrust | 3,350,000 lbf (14,900 kN) |
| Propellant | LCH4 / LOX |
| Second stage | |
| Powered by | 1 Aeon Vac |
| Maximum thrust | 279,000 lbf (1,240 kN) |
| Propellant | LCH4 / LOX |
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