Overview
H11 AERIS-R1 develops research themes spanning rocket burn sequences, telemetry response, heat management, structural stress, and aerospace optimization into a coherent civilian launch-system concept.
H11 Systems
Reusable orbital launch system
H11 AERIS-R1™
A measurable route from ignition through recovery and reuse.
AERIS-R1 is a two-stage research launch architecture organized around instrumented propulsion, explicit flight phases, structural-load limits, thermal management, and recoverable first-stage operations.
Designed around inspectable flight data
Coordinates propulsion, thermal, and structural states
Civilian orbital research and launch focus
System Overview
H11 AERIS-R1™ in context.
What It Does
It places research and commercial payloads into orbit while preserving a complete engineering record of propulsion, guidance, thermal, and structural performance for inspection and iterative reuse.
How It Works
A reusable liquid-propellant first stage carries an expendable or recoverable upper stage. Independent telemetry, guidance, thermal, and load-monitoring channels enforce defined phase transitions and abort criteria.
Capabilities
Operational strengths built into the platform.
This public profile presents the system's capability direction while confidential operating logic and implementation architecture remain protected.
Instrumented staged propulsion
Reusable first-stage architecture
Independent telemetry and health channels
Thermal and structural-load monitoring
Defined recovery and refurbishment workflow
Launch architecture
Integrated with the rest of the H11 stack.
Two-stage liquid-propellant configuration
Explicit burn and flight-phase sequencing
Telemetry-linked vehicle health management
Recoverable booster systems
Applications
Where this system fits.
Research payload launch
Small and medium satellite missions
Responsive civilian launch services
Propulsion and thermal-system validation