Orbital Capabilities
Technical mission parameters
Flight-proven reusability and high-capacity payload capabilities engineered for complex satellite deployment and resilient Asia-Pacific coverage.
Payload Specifications
Fairing volume and precision
Fairing Metrics
Five-meter composite envelope
Acoustic attenuation systems and thermal isolation barriers maintain payload integrity during maximum dynamic pressure and high-altitude orbital insertion.
Orbital Injection
Sub-kilometer target accuracy
Precision cold-gas thrusters and relightable second-stage engines deliver satellites to exact geostationary transfer or low-Earth orbital coordinates.
Power & Telemetry
Regulated high-power interfaces
Standardized umbilical connectors supply up to twenty kilowatts of conditioned power during pre-launch checkout and real-time telemetry integration.
Integration Sequence
Four-phase launch deployment
01
Facility Receiving
Satellite arrival at regional cleanroom facilities for autonomous checkout, propellant loading, and payload adapter fitting.
02
Encapsulation Mating
Mechanical mating to launch vehicle interface, electrical telemetry verification, and final fairing closure under cleanroom controls.
03
Orbital Insertion
Precision launch trajectory execution, second-stage burn sequence, and targeted separation into assigned orbital planes.
04
Constellation Link
Immediate optical inter-satellite routing initialization, ground station lock, and active Asia-Pacific network integration.