 | |
| Function | Reusable orbital launcher |
|---|---|
| Manufacturer | Relativity Space |
| Country of origin | United States |
| Cost per launch | $55 million[1] |
| 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 |
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, like its predecessor, the small-lift Terran 1.[2][3] The first flight is expected to be in 2026.[4]
- ^ "Manhattan Venture Partners | Tomorrow's IPOs Today™".
- ^ Berger, Eric (12 April 2023). "Relativity Space is moving on from the Terran 1 rocket to something much bigger". Ars Technica. Retrieved 12 April 2023.
- ^ "Relativity Space Shares Updated Go-to-Market Approach for Terran R, Taking Aim at Medium to Heavy Payload Category with Next-Generation Rocket". Relativity Space (Press release). 12 April 2023. Retrieved 12 April 2023.
- ^ "Terran R". Relativity Space. Retrieved 2024-02-20.
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