Epsilon (rocket)

JAXA small-lift rocket family From Wikipedia, the free encyclopedia

The Epsilon Launch Vehicle, or Epsilon rocket (イプシロンロケット, Ipushiron roketto) (formerly Advanced Solid 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.[8]

Country of originJapan
Cost per launchUS$39 million[1]
Height24.4 m (E-X)
26 m (Enhanced)
26.8 m (Epsilon S Block1)[2]
27.2 m (Epsilon S)
Quick facts Function, Country of origin ...
Epsilon
Epsilon flight F2 before launch in December 2016
FunctionLaunch vehicle
Country of originJapan
Cost per launchUS$39 million[1]
Size
Height24.4 m (E-X)
26 m (Enhanced)
26.8 m (Epsilon S Block1)[2]
27.2 m (Epsilon S)
Diameter2.5 m
Mass91 t (E-X)
95.4 t (Enhanced)
~100 t (Epsilon S)
Stages3–4
Capacity
Payload to 250 x 500 km orbit
Standard 3 stages configuration
Mass1,500 kg (3,300 lb)
Payload to 500 km orbit
Optional 4 stages configuration
Mass700 kg (1,500 lb)
Payload to 500 km orbit
Epsilon S
Mass1,400 kg (3,100 lb)[3]
Payload to 500 km SSO
Optional 4 stages configuration
Mass590 kg (1,300 lb)
Payload to 700 km SSO
Epsilon S
Mass600 kg (1,300 lb)[3]
Launch history
StatusActive
Launch sitesUchinoura
Total launches6
Success(es)5
Failure1
Partial failure0
First flight14 September 2013
Last flight12 October 2022
First stage (E-X/Enhanced) – SRB-A3
Powered by1 solid
Maximum thrust2,271 kN (511,000 lbf)[4]
Specific impulse284 s (2.79 km/s)
Burn time116 seconds
First stage (Epsilon S Block1/Epsilon S) – SRB-3
Powered by1 solid
Maximum thrust2,158 kN (485,000 lbf)[5]
Specific impulse283.6 s (2.781 km/s)
Burn time105 seconds
Second stage (E-X) – M-34c
Powered by1 solid
Maximum thrust371.5 kN (83,500 lbf)[4]
Specific impulse300 s (2.9 km/s)
Burn time105 seconds
Second stage (Enhanced) – M-35
Powered by1 solid
Maximum thrust445 kN (100,000 lbf)[4]
Specific impulse295 s (2.89 km/s)[6]
Burn time129 seconds[6]
Second stage (Epsilon S Block1) – M-35a
Powered by1 solid
Second stage (Epsilon S) – E-21[3]
Powered by1 solid
Maximum thrust610 kN (140,000 lbf)[3]
Specific impulse294.5 s (2.888 km/s)[3]
Burn time120 seconds[3]
Third stage (E-X) – KM-V2b
Powered by1 solid
Maximum thrust99.8 kN (22,400 lbf)[4]
Specific impulse301 s (2.95 km/s)
Burn time90 seconds
Third stage (Enhanced) – KM-V2c
Powered by1 solid
Maximum thrust99.6 kN (22,400 lbf)[4]
Specific impulse299 s (2.93 km/s)[6]
Burn time91 seconds[6]
Third stage (Epsilon S Block1/Epsilon S) – E-31[7]
Powered by1 solid
Maximum thrust135 kN (30,000 lbf)[7]
Specific impulse~295 s (2.89 km/s)
Burn time108 seconds[7]
Fourth stage (Optional) – PBS
Maximum thrust40.8 N (9.2 lbf)
Specific impulse215 s (2.11 km/s)[4]
Burn time1100 seconds (maximum)
PropellantHydrazine
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Vehicle description

E-X

The development aim is to reduce the US$70 million launch cost of a M-V;[9] the Epsilon costs US$38 million per launch.[10] Development expenditures by JAXA exceeded US$200 million.[10]

To reduce the cost per launch the Epsilon uses the existing SRB-A3, a solid rocket booster on the H-IIA rocket, as its first stage. Existing M-V upper stages will be used for the second and third stages, with an optional fourth stage available for launches to higher orbits. The J-I rocket, which was developed during the 1990s but abandoned after just one launch, used a similar design concept, with an H-II booster and Mu-3S-II upper stages.[11]

The Epsilon is expected to have a shorter launch preparation time than its predecessors;[12][13][14] a function called "mobile launch control" greatly shortens the launch preparation time, and needs only eight people at the launch site,[15] compared with 150 people for earlier systems.[16]

The rocket has a mass of 91 t (90 long tons; 100 short tons) and is 24.4 m (80 ft) tall and 2.5 m (8 ft 2 in) in diameter.[17][18]

Enhanced Epsilon

After the successful launch of the Epsilon first flight (demonstration flight), the improvement plan was decided to handle the planned payloads (ERG and ASNARO-2).[19]

Requirements for the improvement:[19]

  • Apogee ≧ 28700 km (summer launch), ≧ 31100 km (winter launch) of a 365 kg payload
  • Sun-synchronous orbit (500 km) of a ≧ 590 kg payload
  • Larger fairing

Planned characteristics:[19]

  • Height: 26.0 m
  • Diameter: 2.5 m
  • Mass: 95.1 t (Standard) / 95.4 t (Optional 4th stage (Post Boost Stage))

Catalog performance according to IHI Aerospace:[20]

  • Low Earth orbit 250 km × 500 km for 1.5 t
  • Sun-synchronous orbit 500 km × 500 km for 0.6 t

Final characteristics:[8][21]

  • Height: 26.0 m
  • Diameter: 2.6 m (max), 2.5 m (fairing)
  • Mass: 95.4 t (standard) / 95.7 t (optional)

Epsilon S Block1

The Epsilon rocket's first stage has a common design with the SRB-A3, the solid rocket booster of H-IIA/B. As the H-IIA family has retired in 2025, continuing the production of SRB-A3 solely for Epsilon would lead to a significant rise in production cost.[22] Thus a new Epsilon variant, the Epsilon S Block1 which incorporates commonized parts with the H3, the H-IIA's successor, has been in development. The Epsilon S Block1's first stage will have a common design with SRB-3, the H3's solid rocket booster.

Major changes from Enhanced Epsilon to Epsilon S Block1 are:[23]

  • The first stage is based on SRB-3, the strap-on solid rocket booster of H3.
  • The third stage designated the E-31 is a new design, whereas Enhanced Epsilon's third stage was based on the M-V's third stage. New third stage is three-axis stabilized, whereas Epsilon's third stage was spin-stabilized. Also the third stage is outside the fairing, whereas Enhanced Epsilon's fairing covered the third stage.
  • The Epsilon S Block1's forth stage, the Post Boost Stage (PBS) is mandatory, whereas Enhanced Epsilon's PBS was optional.

Epsilon S Block1's second stage, the M-35a will have the same performance as Enhanced Epsilon's M-35, but with changes in propellant and insulation.[2]

In June 2023, a ground test of the E-31 was conducted at JAXA's Noshiro Rocket Testing Center.[24] Ground testing of the M-35a is scheduled to be conducted in 2026 at the Tanegashima Space Center.[2]

Epsilon S

In order to further increase the payload capacity of Epsilon, the Epsilon S Block1's second stage M-35a is planned to be replaced with a larger solid-rocket motor designated E-21.[2]

Initially, the E-21 was to be introduced simultaniously with the SRB-3 first stage and E-31 third stage. However, on 14 July 2023, a test firing of the E-21 failed.[25] The root cause was determined to be the "melting and scattering of a metal part from the ignition device", which damaged the propellant and insulation.[26] Corrective measures were implemented and the rocket motor was tested again on 26 November 26 2024; however, the second test also resulted in a failure 49 seconds after ignition.[27][28][29]

In July 2025, NHK reported that JAXA was reviewing its development plans for the Epsilon S. In order to move up plans for a return to flight, the decison was made to defer planned improvements to the second stage and revert to using the proven, existing design of Enhanced Epsilon. While this would entail performance being lower than originally planned, it could enable a launch as early as late 2026.[30]

Launch statistics

Launch outcomes

1
2013
'14
'15
'16
'17
'18
'19
2020
'21
'22
  •   Failure
  •   Partial failure
  •   Success
  •   Planned

Launch history

Epsilon launch vehicles are launched from a pad at the Uchinoura Space Center previously used by Mu rockets. The first flight, carrying the SPRINT-A scientific satellite, lifted off at 05:00 UTC (14:00 JST) on 14 September 2013. The launch was conducted at a cost of US$38 million.[31]

On 27 August 2013, the first planned launch of the launch vehicle had to be aborted 19 seconds before liftoff because of a botched data transmission. A ground-based computer had tried to receive data from the launch vehicle 0.07 seconds before the information was actually transmitted.[32]

The initial version of Epsilon, E-X had a payload capacity to low Earth orbit of up to 500 kilograms,[33][34] with the Enhanced Epsilon expected to be able to place 1,200 kg (2,600 lb) into a 250 by 500 km (160 by 310 mi) orbit, or 700 kg (1,500 lb) to a circular orbit at 500 km (310 mi) with the aid of a hydrazine fueled stage.[10]

Mockup of Epsilon
More information Flight No., Date / time (UTC) ...
Flight No. Date / time (UTC) Rocket,
Configuration
Launch site Payload Payload mass Orbit Customer Launch
outcome
1 14 September 2013
05:00:00
E-X,
4 Stages[35]
Uchinoura Space Center SPRINT-A (HISAKI) 340 kg LEO JAXA Success
Demonstration Flight
2 20 December 2016
11:00:00[36]
Enhanced Epsilon,
Standard configuration
Uchinoura Space Center ERG (ARASE) 350 kg[37] Geocentric JAXA Success
3 17 January 2018
21:06:11[38]
Enhanced Epsilon,
Optional configuration[39]
Uchinoura Space Center ASNARO-2 570 kg SSO Japan Space Systems Success
4 18 January 2019
00:50:20[40]
Enhanced Epsilon,
Optional configuration
Uchinoura Space Center RAPIS-1
MicroDragon
RISESAT
ALE-1
OrigamiSat-1
AOBA-VELOX-IV
NEXUS
200 kg SSO JAXA Success
Innovative Satellite Technology Demonstration-1; component demonstration and technology validation.[41] A new Guidance and Control system was developed for multiple payload deployment capability.[42]
5 9 November 2021
00:55:16[43][44]
Enhanced Epsilon,
Optional configuration
Uchinoura Space Center RAISE-2
HIBARI
Z-Sat
DRUMS
TeikyoSat-4
ASTERISC
ARICA
NanoDragon
KOSEN-1
110 kg SSO JAXA Success
Innovative Satellite Technology Demonstration-2.
6 12 October 2022
00:50:00[45]
Enhanced Epsilon,
Optional configuration
Uchinoura Space Center RAISE-3
QPS-SAR 3
QPS-SAR 4
MAGNARO
MITSUBA
KOSEN-2
WASEDA-SAT-ZERO
FSI-SAT
110 kg SSO JAXA, iQPS Failure
RAISE-3 and the six CubeSats were part of Innovative Satellite Technology Demonstration-3. QPS-SAR 3/4 were Epsilon's first commercial satellites launch contracts. Vehicle was destroyed by flight termination system shortly after second stage cutoff due to an attitude control fault.[45][46] A report regarding the cause has been published and is available for viewing, although it is in Japanese.[47]
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Planned launches

More information Date / time (UTC), Rocket, Configuration ...
Date / time (UTC) Rocket,
Configuration
Launch site Payload Orbit Customer
2026[2] Epsilon S Block1 Uchinoura Space Center TBD TBD JAXA
TBD Epsilon S Block1 Uchinoura Space Center LIDAR Altimeter Satellite[2] SSO JAXA
TBD Epsilon S Block1 Uchinoura Space Center TBD (JAXA-STEPS rideshare)[2] TBD JAXA
TBD Epsilon S Block1 Uchinoura Space Center LOTUSat-1[48] SSO VNSC
July 2028[49] Epsilon S Uchinoura Space Center Solar-C[50][51] SSO JAXA
November 2028[52] Epsilon S Kick Stage[53] Uchinoura Space Center OPENS-0 TBD JAXA
2032[54] Epsilon S Uchinoura Space Center JASMINE[55] SSO JAXA
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Sources: Cabinet Office of Japan[54]

Internet data leak

In November 2012, JAXA reported that there had been a possible leak of rocket data due to a computer virus. JAXA had previously been a victim of cyber-attacks, possibly for espionage purposes.[56] Solid-fuel rocket data potentially has military value,[56] and Epsilon is considered as potentially adaptable to an intercontinental ballistic missile.[57] The Japan Aerospace Exploration Agency removed the infected computer from its network, and said its M-V rocket and H-IIA and H-IIB rockets may have been compromised.[58]

See also

References

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