Epsilon test flight | Enhanced Epsilon | ||||
---|---|---|---|---|---|
Basic formfactor |
Optional formfactor |
Basic formfactor |
Optional formfactor |
||
Specifications | Total length |
Approximately 24.4m | Approximatel 26.0m | ||
Diameter | Φ2.6m | ||||
Total mass | Approximately 91.0t | Approximately 92.0t | Approximately 95.4t | Approximately 95.7t | |
Satellite envelope |
Approximately 4.7m | Approximately 5.4m | |||
Staged construction |
Solid three stage | Solid three stage+ Small formfactor liquid propulsion system |
Solid three stage | Solid three stage+ Small formfactor liquid propulsion system |
|
Launch performance |
Low Earth orbit (LEO) |
1200kg (250km×500km) |
700kg (500km circular orbit) |
ー | |
Sun-synchronous orbit (SSO) |
ー | 450kg (500km circular orbit) |
ー | 590kg+ (500km circular orbit) |
|
Extended elliptica orbit |
ー | 365kg+ (approx. 200km x 30,000km) |
ー |
©Japan Aerospace Exploration Agency