Small Reusable Launch Vehicle (SRLV)
abyom-spacetech
Orbital small launch vehicle with 2.6 t to LEO (reusable) or 7 t (expendable) — 9× AbyoKalam-350 LOX/LNG engines, 55 m tall, targeting commercial small satellite operators.
Technical specifications
- Height
- 55 m
- Diameter
- 3 m
- Payload (reusable) to LEO
- 2.6 t
- Payload (reusable) to SSO
- 1 t
- Payload (expendable) to LEO
- 7 t
- Payload (expendable) to SSO
- 5 t
- Propellant
- LOX/LNG
- Engine model
- AbyoKalam-350
- Number of engines
- 9
About
Abyom SpaceTech’s Small Reusable Launch Vehicle (SRLV) is a 55 m tall, 3 m diameter orbital launcher optimized for frequent commercial deployment of small satellites and constellations. In reusable mode it delivers 2.6 tonnes to LEO and 1 tonne to SSO; expendable operations extend capacity to 7 tonnes to LEO and 5 tonnes to SSO. The vehicle is powered by nine AbyoKalam-350 engines burning LOX/LNG propellant, enabling high efficiency with clean combustion. Reusable first stage recovery compresses turnaround time and reduces per-launch cost for commercial constellation builders in the Indian and global market.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.
