Mission V-9 Active

ENGINEERING
THE ORBITAL
FRONTIER.

Developing next-generation heavy-lift launch vehicles and deep space orbital habitats. Precision engineering for the commercialization of low Earth orbit.

Live Telemetry
Altitude (KM) 408.92
Velocity (KM/S) 7.66
Inclination 51.6°
Propellant
84%
T-Minus 00:14:28:09

Contracted by premier aerospace entities

ESA NASA JPL DARPA AIRBUS

CORE SYSTEMS

Modular architecture designed for rapid deployment and maximum payload mass fraction.

View Specifications →

Launch Vehicles

Fully reusable medium to heavy-lift launch systems optimized for high-cadence orbital delivery.

Aether-Heavy // Block II

Satellite Buses

Standardized modular satellite platforms supporting electro-optical and synthetic aperture radar payloads.

Nexus Platform

Orbital Logistics

In-space transportation, active debris removal, and satellite life-extension servicing vehicles.

Tug-V1 Active
FIG. 01
METHALOX // STAGED COMBUSTION

PROPULSION
REDEFINED.

Our proprietary Aeon-X engine utilizes closed-cycle staged combustion for unprecedented specific impulse. Manufactured entirely via directed energy deposition (3D printing), reducing part count from thousands to tens.

Additive Manufacturing

Continuous print volumes up to 12 meters, allowing for unibody tank structures without traditional weld seams.

Methalox Architecture

Liquid Oxygen and liquid Methane propellants enable clean burning, deep throttling, and in-situ resource utilization potential on Mars.

LAUNCH MANIFEST

Schedule subject to range availability

Mission ID Payload Orbit Vehicle Target Date Status
AET-24A Starlink Group 10-1 LEO (53.0°) Aether Heavy (B104) Q3 2024 Go
AET-24B NROL-118 GEO Aether Heavy (B101) Q4 2024 Processing
AET-25A Artemis Support Module TLI Aether Super-Heavy Q1 2025 Manifested

MISSION LIFECYCLE

Payload Integration

Cleanroom Class 100K processing.

Rollout & Pad Ops

Transport to LC-39A. Wet dress rehearsal.

Terminal Count

Auto-sequence start. Engine ignition.

Max-Q & SECO

Maximum dynamic pressure. Stage separation.