- Space Transportation Systems
- « Operation »
- H-IIB Launch Vehicle
- H-IIA Launch Vehicle
- KOUNOTORI (HTV)
- S-310/S-520/SS-520
- « Development »
- Epsilon Launch Vehicle
- LNG Propulsion System
- Human Space Activities
- Satellites & Spacecraft
- Utilization with Satellites
- Space Science Research
- Basic Technology Research
- Aviation Program
- Past Projects
Here are charts and drawings showing the major characteristics and launch capability of Epsilon.
Epsilon Major Characteristics
| Length (m) | 24 |
|---|---|
| Mass (t) | 91 |
Epsilon Launch Vehicle Launch Capacity
| Specifications | Standard Configuration Three-staged Solid Propellant Launch Vehicle | Optional Configuration Three-staged Solid Propellant Launch Vehicle + Compact Liquid Propulsion System |
|---|---|---|
| Low Earth Orbit (LEO) | 1200kg (Perigee 250km x Apogee 500km) |
700kg (500km circle) |
| Sun-Synchronous Orbit (SSO) | - | 450kg (500km circle) |
