Orbital launch vehicle
Epsilon
The Epsilon rocket is a Japanese solid-fuel rocket designed to launch scientific satellites. It is a follow-on project to the larger and more expensive M-V rocket which was retired in 2006. The Japan Aerospace Exploration Agency (JAXA) began developing the Epsilon in 2007. It is capable of placing a 590 kg payload into Sun-synchronous orbit.
Flights flown6
Success rate83.3%5/6
Maiden flight2013-09-14
Peak year20131 flight
Epsilon is built by Japan Aerospace Exploration Agency of Japan. It first flew on 14 September 2013.
Flight record
83.3% success rate5 of 6 flown · 1 failed
2013peak 2013 · 1 flight2022
First flight2013-09-14
Latest flight2022-10-12
Failures1
Consecutive successes0
Fastest turnaround336d 23h
Payload
| Sun-synchronous orbit | 590kg |
|---|---|
| Launch cost | $39M |
Vehicle
| Stages | 4 |
|---|---|
| Length | 24.4m |
| Diameter | 2.5m |
| Launch mass | 91t |
| Liftoff thrust | 2,271kN |
| Maiden flight | 2013-09-14 |
| Reusable | No |
Pads used
Orbits delivered
Sun-Synchronous Orbit3Low Earth Orbit2Elliptical Orbit1
Launch history
| Date | Mission | Pad | Orbit | Outcome |
|---|---|---|---|---|
| 2022-10-12 | Epsilon | RAISE-3 & others | Mu Center | Sun-Synchronous Orbit | Failure |
| 2021-11-09 | Epsilon | RAISE-2 & others | Mu Center | Low Earth Orbit | Success |
| 2019-01-18 | Epsilon | RAPIS-1 & others | Mu Center | Sun-Synchronous Orbit | Success |
| 2018-01-17 | Epsilon | ASNARO-2 | Mu Center | Sun-Synchronous Orbit | Success |
| 2016-12-20 | Epsilon | ERG (ARASE) | Mu Center | Elliptical Orbit | Success |
| 2013-09-14 | Epsilon | Hisaki (SPRINT-A) | Mu Center | Low Earth Orbit | Success |
Specifications from Launch Library 2 by The Space Devs, launch records from Space Index. Derived figures are computed here; see sources and method.
Further reading: Wikipedia