Miura 5

Miura 5
A reuse test small-scale first stage of Miura 5 in El Arenosillo
Functionpartially reusable launch vehicle to low Earth orbit
ManufacturerPLD Space
Country of originSpain
Size
Height35.7 m (117 ft)
Diameter2.0 m (6 ft 7 in)
Mass
  • 69,025 kg
Stages2–3
Capacity
Payload to Low Earth orbit (LEO)
Mass1,080 kg (2,380 lb)
Payload to SSO
Mass540 kg (1,190 lb)
Associated rockets
ComparableShavit 2, Prime, Electron
Launch history
StatusUnder development
Launch sitesEl Hierro Launch Centre (proposed)

Guiana Space Centre (planned)

Azores (proposed)
First flightQ1 2026 (planned)
First stage
Height26.3 m (86 ft)
Diameter2.0 m (6 ft 7 in)
Powered by5 TEPREL-C
Maximum thrust950 kN (210,000 lbf)
Burn time182 s.
PropellantLOX / RP-1
Second stage
Height12.1 m (40 ft)
Powered by1 TEPREL-C vacuum
Maximum thrust50 kN (11,000 lbf)
Burn time420 s.
PropellantLOX / RP-1
Kick stage (optional)

Miura 5 is a two-stage European orbital recoverable launch vehicle currently under development by the Spanish company PLD Space. In a standard two-stage configuration, it will have a length of 34 m, be capable of inserting 1000 kg of payload into a low Earth orbit (LEO), featuring an optional kick stage that can circularize the orbits of satellites.

Development of the Miura 5 has been sponsored by the European Space Agency (ESA) via the agency's Future Launchers Preparatory Programme (FLPP); additional support has come from the French space agency CNES and the Spanish agency National Institute for Aerospace Technology (INTA). Work commenced during the mid-2010s under the name Arion 2, the present name was adopted following a redesign that doubled the lift capacity of the launcher during 2018. On 11 April 2019, PLD Space carried out a successful drop and recovery test of the first stage of a Miura 5 demonstrator. As of February 2025, the first test flight of Miura 5 is expected to take place sometime in early 2026.