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Terran-R
Terran-R [Relativity Space] |
The Terran-R is a planned partially reusable launch vehicle by Relativity Space, which will be built mostly by 3D printing.
The vehicle is a two-stage, 82.3-meter-tall rocket with a 5.5-meter diameter and a 5-meter payload fairing. It features a reusable first stage powered by 13 Aeon-R engines running on Methane and LOX. The expendable second stage is powered by a single Aeon-R-Vacuum engine.
Originally Terran-R was planned to be fully reusable, but during development the second stage was changed to an expendable design.
The maiden flight is planned for 2026.
| Launch Vehicle | Stage 1 | Stage 2 |
|---|---|---|
| Terran-R | Stg 1 / 13 × Aeon-R | Stg 2 / Aeon-R-Vacuum |
| Performance (kg) | LEO | LPEO | SSO | GTO | GEO | MolO | IP |
|---|---|---|---|---|---|---|---|
| Terran-R | 23500 | 5500 | |||||
| Terran-R (ex) | 33500 |
Nr: TNr: Vehicle: Serial: Fair: LS: Date: Payload
none Planned: 1 1 Terran-R ? xx.xx.2026 ? x x Terran-R ? xx.xx.202x OneWeb Gen-2 (unk. no. of satellites, unknown number of launches) x x Terran-R ? xx.xx.2026 Intelsat (unknown number of launches) Launch sites: CC = Cape Canaveral Air Force Station, Eastern Test Range, Cape Canaveral, Florida, USAVa = Vandenberg Air Force Base, California, USA
