RPS Suborbital Launch Vehicle
Rocket Propulsion Systems (RPS)
Single-stage reusable VTVL suborbital test vehicle reaching 50-100km altitude.
Technical specifications
- Stages
- single-stage, VTVL
- Target apogee
- 50-100 km
- Prototype testing
- targeted 2026
About
The RPS Suborbital Launch Vehicle is a single-stage, fully reusable vertical-takeoff-vertical-landing (VTVL) vehicle powered by the Centurion LOX/methane engine, designed to reach altitudes of roughly 50 to 100km for microgravity research, hypersonic testing, and technology demonstration missions. Guided and unguided variants are planned, with prototype flight testing targeted for 2026.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.
