Launch Cadence Engine
Baseline 2026
Delta-V & Lunar Mass Calculator
US Net Lunar Surface Payload
48.5 t
CN Net Lunar Surface Payload
27.0 t
United States (NASA/SpaceX/DoD)
China (CNSA/CASC/Commercial)
Target Year: 2026
Strategic Space Parity
US Tonnage Advantage
US Annual LEO Mass
1,680 t
CN Annual LEO Mass
245 t
US Artemis Crewed Target
2027
China ILRS Crewed Target
2030
Architectural Assessment & Bottlenecks:
US maintains heavy lift dominance via Starship rapid reusability and commercial launch frequency. China is rapidly closing the gap in launch cadence (Long March 5/10) with planned 2030 crewed lunar landing parity.
Flight Architecture Manifest
| System | Country | Payload (LEO) | Status |
|---|