Terran R

In Development
Relativity Space
Relativity Space
Terran R

Overview

A two-stage reusable medium-to-heavy-lift rocket designed for constellation deployment, large satellite missions, and higher-cadence commercial and government launch operations.

In integrated vehicle build and testing as of mid-August 2026: the stage-one structural qualification campaign is complete, the flight-one second stage completed cryoproof and COPV manifold proof testing at NASA Stennis's A-2 test stand, and all Flight 1 engines (13 Aeon R first-stage engines plus the Aeon V second-stage engine) have completed acceptance testing. The first Aeon R engines are now being installed onto the first-stage thrust structure at Long Beach, and the LC-16 Horizontal Integration Facility at Cape Canaveral is structurally complete with pad infrastructure (water tower, flame diverter, lightning protection towers, transporter-erector) continuing to come online. First launch is targeted for the second half of 2026 (some observers expect a slip into 2027).

Key Specs

Payload to LEO

23,500 kg (downrange landing)

Height

86.6 m (284 ft)

Diameter & Payload Fairing

5.4 m (17.7 ft)

Total Liftoff Thrust

3,497,000 lbf

Engines

13 × Aeon R (LOx/methane, ~258,000 lbf SL each) + 1 × Aeon V vacuum

Target First Launch

Late 2026