Relativity Space Advances Terran R Reusable Launch Vehicle for LEO Constellations

Relativity Space Advances Terran R Reusable Launch Vehicle for LEO Constellations

Relativity Space is developing Terran R, a fully reusable, two-stage launch vehicle designed to provide reliable, routine, and cost-effective access to space for commercial, government and scientific missions. Optimized for the growing Low Earth Orbit (LEO) satellite constellation market while supporting missions beyond LEO, Terran R is intended to expand launch capacity for next-generation communications, Earth observation, exploration and research payloads. The vehicle is currently in progress for its launch from Launch Complex 16 at Cape Canaveral Space Force Station in Florida.

Terran R measures 86.6 m (284 ft) in height with a 5.4 m (17.7 ft) diameter, including its payload fairing. The launch vehicle generates approximately 3.5 million pounds-force (15.56 MN) of liftoff thrust and is designed to deliver up to 23500 kg to Low Earth Orbit (LEO) in its reusable downrange landing configuration, 5,500 kg to Geosynchronous Transfer Orbit (GTO), or 33500 kg to LEO when flown in an expendable configuration. These capabilities position the vehicle to support a broad range of dedicated satellite deployment and exploration missions.

The propulsion system consists of 13 Aeon R engines powering the reusable first stage and a single Aeon V vacuum engine on the second stage. Both engines utilize liquid oxygen (LOX) and liquid methane propellants with a high-pressure gas generator cycle to maximize performance, efficiency, and operational reliability. Each Aeon R engine produces approximately 269,000 lbf of sea-level thrust, while the Aeon V engine delivers around 323000 lbf of vacuum thrust. Relativity Space notes that the Aeon R engine progressed from design to qualification in just 14 months, demonstrating rapid propulsion development.

A major feature of Terran R is its reusable architecture combined with cost-effective manufacturing. The launch vehicle is constructed using high-strength aluminum alloys that are designed to provide competitive launch economics while supporting large payload capacities and repeated flight operations. The payload fairing accommodates a wide range of mission configurations, including single ESPA Grande payloads, dual ESPA deployments and multi-CubeSat rideshare missions, while a flight-proven thermal protection system safeguards spacecraft until fairing separation during ascent.

Terran R is designed to improve launch availability for customers requiring dedicated access to specific orbital destinations without relying on rideshare opportunities. The vehicle supports rapid deployment of satellite constellations and enables spacecraft to reach custom orbital parameters more quickly. Terran R has already secured more than US$3 billion in launch service agreements with government, commercial and telecommunications customers, reflecting strong demand for its reusable launch capabilities.

By combining full first-stage reusability, methane-fueled propulsion, high payload capacity and scalable launch operations, Terran R is designed to support the next generation of commercial satellite constellations, scientific exploration and deep-space missions. Relativity Space aims to make access to space more reliable and routine while enabling future innovation across Earth orbit and beyond.

About Relativity Space

Relativity Space is a U.S.-based aerospace company headquartered in Long Beach, California. The company develops reusable launch vehicles and advanced aerospace manufacturing technologies to expand access to space. Its flagship launch system, Terran R, is designed to support commercial, government, scientific and exploration missions through reusable rocket technology, advanced propulsion systems and efficient launch operations.

Click here to learn more about Relativity Space's Terran R 

Publisher: SatNow

GNSS Constellations - A list of all GNSS satellites by constellations

beidou

Satellite NameOrbit Date
BeiDou-3 G4Geostationary Orbit (GEO)17 May, 2023
BeiDou-3 G2Geostationary Orbit (GEO)09 Mar, 2020
Compass-IGSO7Inclined Geosynchronous Orbit (IGSO)09 Feb, 2020
BeiDou-3 M19Medium Earth Orbit (MEO)16 Dec, 2019
BeiDou-3 M20Medium Earth Orbit (MEO)16 Dec, 2019
BeiDou-3 M21Medium Earth Orbit (MEO)23 Nov, 2019
BeiDou-3 M22Medium Earth Orbit (MEO)23 Nov, 2019
BeiDou-3 I3Inclined Geosynchronous Orbit (IGSO)04 Nov, 2019
BeiDou-3 M23Medium Earth Orbit (MEO)22 Sep, 2019
BeiDou-3 M24Medium Earth Orbit (MEO)22 Sep, 2019

galileo

Satellite NameOrbit Date
GSAT0223MEO - Near-Circular05 Dec, 2021
GSAT0224MEO - Near-Circular05 Dec, 2021
GSAT0219MEO - Near-Circular25 Jul, 2018
GSAT0220MEO - Near-Circular25 Jul, 2018
GSAT0221MEO - Near-Circular25 Jul, 2018
GSAT0222MEO - Near-Circular25 Jul, 2018
GSAT0215MEO - Near-Circular12 Dec, 2017
GSAT0216MEO - Near-Circular12 Dec, 2017
GSAT0217MEO - Near-Circular12 Dec, 2017
GSAT0218MEO - Near-Circular12 Dec, 2017

glonass

Satellite NameOrbit Date
Kosmos 2569--07 Aug, 2023
Kosmos 2564--28 Nov, 2022
Kosmos 2559--10 Oct, 2022
Kosmos 2557--07 Jul, 2022
Kosmos 2547--25 Oct, 2020
Kosmos 2545--16 Mar, 2020
Kosmos 2544--11 Dec, 2019
Kosmos 2534--27 May, 2019
Kosmos 2529--03 Nov, 2018
Kosmos 2527--16 Jun, 2018

gps

Satellite NameOrbit Date
Navstar 82Medium Earth Orbit19 Jan, 2023
Navstar 81Medium Earth Orbit17 Jun, 2021
Navstar 78Medium Earth Orbit22 Aug, 2019
Navstar 77Medium Earth Orbit23 Dec, 2018
Navstar 76Medium Earth Orbit05 Feb, 2016
Navstar 75Medium Earth Orbit31 Oct, 2015
Navstar 74Medium Earth Orbit15 Jul, 2015
Navstar 73Medium Earth Orbit25 Mar, 2015
Navstar 72Medium Earth Orbit29 Oct, 2014
Navstar 71Medium Earth Orbit02 Aug, 2014

irnss

Satellite NameOrbit Date
NVS-01Geostationary Orbit (GEO)29 May, 2023
IRNSS-1IInclined Geosynchronous Orbit (IGSO)12 Apr, 2018
IRNSS-1HSub Geosynchronous Transfer Orbit (Sub-GTO)31 Aug, 2017
IRNSS-1GGeostationary Orbit (GEO)28 Apr, 2016
IRNSS-1FGeostationary Orbit (GEO)10 Mar, 2016
IRNSS-1EGeosynchronous Orbit (IGSO)20 Jan, 2016
IRNSS-1DInclined Geosynchronous Orbit (IGSO)28 Mar, 2015
IRNSS-1CGeostationary Orbit (GEO)16 Oct, 2014
IRNSS-1BInclined Geosynchronous Orbit (IGSO)04 Apr, 2014
IRNSS-1AInclined Geosynchronous Orbit (IGSO)01 Jul, 2013
Advertisement