Medium Reusable Launch Vehicle (MRLV)
abyom-spacetech
Heavy-lift orbital launch vehicle — 15 t to LEO (reusable) or 2 t to GTO — 75 m tall, 9× AbyoKalam-950 LOX/LNG engines for telecom, defense, and cargo missions.
Technical specifications
- Height
- 75 m
- Diameter
- 4.8 m
- Payload (reusable) to LEO
- 15 t
- Payload (reusable) to SSO
- 9 t
- Payload (reusable) to GTO
- 2 t
- Propellant
- LOX/LNG
- Engine model
- AbyoKalam-950
- Number of engines
- 9
About
Abyom SpaceTech’s Medium Reusable Launch Vehicle (MRLV) is a heavy-lift system standing 75 m tall (4.8 m diameter) for high-value missions including geostationary telecom satellites, defense payloads, and crew/cargo transport. In reusable configuration it lifts 15 tonnes to LEO, 9 tonnes to SSO, and 2 tonnes to GTO. Nine AbyoKalam-950 LOX/LNG engines provide the necessary thrust. The reusable first stage drives down economics for high-mass missions and supports India’s sovereign GTO capability for independent geostationary satellite deployment.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.
