PLD Space enters new phase as Miura 5 tests begin
- Miura 5 is a two-stage, small-lift rocket using kerosene and liquid oxygen, with listed payloads of 1 tonne and 540 kilograms.
- PLD Space has completed stage-separation testing and fairing qualification models, and first-flight hardware includes liquid oxygen tanks for both stages.
- The second stage is fully integrated and installed vertically in Teruel, with a static hot-fire test listed as part of qualification.
- A first launch is listed for 2027 from Guiana Space Centre, where PLD Space has a CNES partnership.
- TEPREL-C and TEPREL-C Vac engines are manufactured and beginning test campaigns, while partial reusability is planned for later versions.
What happened
PLD Space has entered a new phase ahead of a first demonstration flight. Miura 5 is beginning system-level test campaigns.
What we know
Miura 5 is listed as a two-stage, small-lift vehicle using kerosene and liquid oxygen.
Payload entries are 1 tonne and 540 kilograms, and the listed orbits are equatorial low Earth orbit and sun-synchronous orbit.
The launch site is Guiana Space Centre (CSG), and PLD Space has a partnership with CNES.
Stage-separation testing is complete and verified interfaces, commands and timing sequence. Fairing qualification models are complete, and the reference trajectory is consolidated.
First-flight hardware has been manufactured, including liquid oxygen tanks for both stages.
The second stage has reached full integration, was installed vertically in Teruel, and has a static hot-fire test listed.
Why it matters
For readers tracking the lunar industry, the facts identify a small-lift vehicle with 1 tonne and 540 kilograms payload entries, equatorial low Earth orbit and sun-synchronous orbit options, a Guiana Space Centre (CSG) launch site, and a CNES partnership. The recorded tests and integration steps provide concrete development checkpoints.
What's next
The launch date is listed as 2027.
Miura 5 is beginning system-level test campaigns. The second stage is entering a qualification campaign, and a Wet Dress Rehearsal is listed.
TEPREL-C and TEPREL-C Vac engines are manufactured and beginning test campaigns. Strongback validation is progressing, and partial reusability is planned for later versions.
What we are not sure about
- The payload facts do not state which mass applies to which listed orbit.
- The launch date is given only as 2027.
Sources
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