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Hardware/Vehicles/M-V

M-V

Retired

ISAS / JAXA · 3-stage orbital rocket

Total Launches
7
Success Rate
85.7%
Payload to LEO
1.8 t
First Flight
1997
Reusable
No

Specifications

Height30.7 m
Diameter2.5 m
Wet Mass139,000 kg
Payload to GTON/A
Payload to SSON/A
ManufacturerISAS / JAXA
CountryJapan

Engines Used

No engine records tracked for this vehicle yet.

    Engine usage data lives in the Engine Dashboard.

    Launch History

    Reliability by Year

    Related Entities

    ISAS / JAXAManufacturer

    Data Sources for This Record

    Specifications
    GCAT / Wikipedia · verified quarterly
    Launch History
    LL2 API · updated every 6h
    Engine Data
    Manufacturer + Wikidata