Reusable Sounding Rocket
abyom-spacetech
Two-stage reusable sounding rocket delivering 200 kg to LEO — 5× AbyoKalam-35 LOX/LNG engines, 16 m booster, designed for atmospheric research and microgravity experiments.
Technical specifications
- Payload capacity
- 200 kg to LEO
- Booster stage
- 16 m height × 1.8 m diameter
- Payload stage
- 16 m height × 2 m diameter
- Propellant
- LOX/LNG
- Engine model
- AbyoKalam-35
- Number of engines
- 5
- Reusable
- Yes
About
Abyom SpaceTech’s Reusable Sounding Rocket is a two-stage launch platform for cost-effective, frequent access to near-space and orbital environments. The booster stage stands 16 m tall (1.8 m diameter) and the payload stage is 16 m tall (2 m diameter), with a 200 kg payload capacity to LEO. Propulsion is provided by a cluster of five AbyoKalam-35 engines burning LOX/LNG propellant. The platform serves scientific agencies, universities, and startups conducting meteorological studies, upper atmospheric research, life sciences, and material validation experiments in microgravity. Reusability is a core design principle to reduce per-mission costs and enable higher launch cadence.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.
