Launcher

Terran 1

Dedicated smallsat launcher designed for 1479 kg to Low Earth Orbit and 898 kg to Sun-Synchronous Orbit.

Launcher Info

Status
No Longer in Use
Maximum Performance
Small-Lift
Type
Rocket Launcher
Reusability

Launcher Cofigurations

Related Links

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Additional Background

Following the same model as several other launch companies (RocketLab, SpaceX), Relativity used a single engine design (Aeon) on Terran 1, with nine Aeon engines on the booster, and a single vacuum-optimized Aeon engine on the upper stage. Terran 1 was built entirely from 3D-printed parts, including tanks, engines, bulkheads, and all other parts of the booster and second-stage.

Terran 1 was abandoned after its first launch, with the company pivoting to the more powerful Terran R. This occurred during a time in the industry when dedicated smallsat launchers were experiencing market pressure. Before cancellation, there was discusion of replacing the nine Aeon engines on the first stage with a single Aeon-R engine; this option was ultimately not pursued.

Launches From

Engines

Common Payloads

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Company

Operated By

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Service History

Development History

Launch Manifest

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Launch History

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9 Aeon-1
Initial configuration using a nine Aeon-1 engines on the first stage.
Configuration Service Status
Development Suspended
Mass to LEO Classification
Small-Lift
Performance
Orbit
Mass to Orbit (kg)
Low-Earth Orbit (LEO)
No Data
Sun-Synchronous Orbit (SSO)
No Data
Geostationary Transfer Orbit (GTO)
No Data
Geostationary Orbit (GSO)
No Data
Lunar Transfer Orbit (LTO)
No Data
Mars Transfer Orbit (MTO)
No Data
Specs
Orbit
Mass to Orbit (kg)
Length
No Data
Diameter
No Data
Dry Mass
No Data
Pressurized Volume
No Data
No detailed launcher stage information is available.
1 Aeon-R
Proposed configuration using a single 1 Aeon-R engine on the first-stage.
Configuration Service Status
Development Suspended
Mass to LEO Classification
Small-Lift
Performance
Orbit
Mass to Orbit (kg)
Low-Earth Orbit (LEO)
No Data
Sun-Synchronous Orbit (SSO)
No Data
Geostationary Transfer Orbit (GTO)
No Data
Geostationary Orbit (GSO)
No Data
Lunar Transfer Orbit (LTO)
No Data
Mars Transfer Orbit (MTO)
No Data
Specs
Orbit
Mass to Orbit (kg)
Length
No Data
Diameter
No Data
Dry Mass
No Data
Pressurized Volume
No Data
No detailed launcher stage information is available.