Epsilon CLPS (SPRINT A) [JAXA]
Epsilon (2) (ERG) [JAXA]
Epsilon (2) CLPS (ASNARO 2) [JAXA]
The Epsilon (designated Advanced Solid Rocket during development) is the replacement for the M-5 rocket.
The initial configuration, Epsilon, featured the SRB-A3 Booster of the H-2A as first stage and the M-34c and KM-V2b stages of M-5 heritage as second and third stages. Two SMSJ ( Solid Motor Side Jet) are added to the SRB-A motor for roll control. Optionally, a liquid fueled fourth stage (CLPS, Compact Liquid Propulsion Stage) can be carried. It will be capable to put about 1200 kg into low earth orbit (3 stage) or 450 kg into a sun synchronous orbit (4 stage). The focus in development will be on streamlining the launch procedures and reducing the costs.
Beginning with the second flight, it was replaced by the improved Epsilon (2) (Enhanced Epsilon), which features the larger M-35 stage 2 and a modified stage 3 KM-V2c, which both will have non-extending nozzles to improve performance and to simplify the vehicle.
The new rocket had its maiden flight in 2013.
|Version||Stage 1||Stage 2||Stage 3||Stage 4|
|Epsilon CLPS||SRB-A3 + 2 × SMSJ||M-34c||KM-V2b||CLPS|
|Epsilon (2) (Enhanced Epsilon)||SRB-A3 + 2 × SMSJ||M-35||KM-V2c||-|
|Epsilon (2) imp. CLPS (Enhanced Epsilon imp. CLPS)||SRB-A3 + 2 × SMSJ||M-35||KM-V2c||imp. CLPS|
|Epsilon (2) (Enhanced Epsilon)||1500||-||-||-||-||-||-|
|Epsilon (2) imp. CLPS (Enhanced Epsilon imp. CLPS)||-||590||-||-||-||-|
No: Serial: Type: Date: LS Payload
1 1 Epsilon CLPS 14.09.2013 Ka LP-M EXCEED (SPRINT A) 2 1 Epsilon (2) 20.12.2016 Ka LP-M ERG (SPRINT B) 3 1 Epsilon (2) CLPS 17.01.2018 Ka LP-M ASNARO 2 Planned: 4 2 Epsilon (2) CLPS xx.xx.2018 Ka LP-M Innovative technology demonstration satellite 1 / ALE 1 / Hodoyoshi 2 / MicroDragon / OrigamiSat 1 / AOBA-VELOX 4 / NEXUS x x Epsilon (2) CLPS xx.xx.2018 Ka LP-M JV-LOTUSat 1 Launch sites: Ka = Kagoshima Space Center / Uchinoura Space Center, Kagoshima, Kyushu, Japan