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

6 records
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

Per mission profile
Sun-synchronous orbit590kg
Launch cost$39M

Vehicle

Stages4
Length24.4m
Diameter2.5m
Launch mass91t
Liftoff thrust2,271kN
Maiden flight2013-09-14
ReusableNo

Pads used

1 pad

Orbits delivered

3 orbits
Sun-Synchronous Orbit3Low Earth Orbit2Elliptical Orbit1

Launch history

6 launches
DateMissionPadOrbitOutcome
2022-10-12Epsilon | RAISE-3 & othersMu CenterSun-Synchronous OrbitFailure
2021-11-09Epsilon | RAISE-2 & othersMu CenterLow Earth OrbitSuccess
2019-01-18Epsilon | RAPIS-1 & othersMu CenterSun-Synchronous OrbitSuccess
2018-01-17Epsilon | ASNARO-2Mu CenterSun-Synchronous OrbitSuccess
2016-12-20Epsilon | ERG (ARASE)Mu CenterElliptical OrbitSuccess
2013-09-14Epsilon | Hisaki (SPRINT-A)Mu CenterLow Earth OrbitSuccess

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