Miura family
Miura 5
MIURA 5 is a 2 stage launch vehicle powered by liquid oxygen and kerosene. The vehicle is designed, integrated and operated by PLD Space, and its 1st stage is designed to be eventually recovered by parachuting into the sea.
Flights flown02 scheduled
Payload to LEO900kg
Peak year20261 flight
Miura 5 is built by Payload Aerospace S.L. of Spain. Company background, funding, contracts and news for this operator are tracked on Space Index.
Payload
| Low Earth orbit | 900kg |
|---|---|
| Sun-synchronous orbit | 540kg |
Vehicle
| Stages | 3 |
|---|---|
| Length | 35.81m |
| Diameter | 2m |
| Liftoff thrust | 950kN |
| Reusable | Yes |
Pads used
Orbits delivered
Low Earth Orbit1Sun-Synchronous Orbit1
Launch history
| Date | Mission | Pad | Orbit | Outcome |
|---|---|---|---|---|
| TBD | Miura 5 | Maiden Flight | Diamant Launch Area | Sun-Synchronous Orbit | Scheduled |
| TBD | Miura 5 | 2 x Tritó | Diamant Launch Area | Low Earth Orbit | Scheduled |
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 · Operator page
Fewer than three recorded flights, so this page is marked noindex. It is here for completeness, not for search.