H-IIA 202
RetiredNASDA / MHI · 2-stage orbital rocket · Part of the H2 family
Total Launches
35
Success Rate
100%
Payload to LEO
10 t
First Flight
2001
Reusable
No
Interactive Model
Specifications
Height53 m
Diameter4 m
Wet Mass285,000 kg
Payload to GTO4.1 t
Payload to SSON/A
ManufacturerNASDA / MHI
CountryJapan
Engines Used
Engine usage data lives in the Engine Dashboard.
Launch History
Reliability by Year
Related Entities
Data Sources for This Record
Specifications
GCAT / Wikipedia · verified quarterly
Launch History
LL2 API · updated every 6h
Engine Data
Manufacturer + Wikidata