# Miura 5

> orbital recoverable small-lift launch vehicle developed by Spanish company PLD Space

**Wikidata**: [Q50322465](https://www.wikidata.org/wiki/Q50322465)  
**Wikipedia**: [English](https://en.wikipedia.org/wiki/Miura_5)  
**Source**: https://4ort.xyz/entity/miura-5

## Summary
Miura 5 is an orbital, recoverable small-lift launch vehicle developed and manufactured by the Spanish company PLD Space. It is a two-stage-to-orbit, reusable rocket in the Miura family designed to place small payloads into low Earth orbits, with a launch mass of about 69,025 kg and standing 35.7 m tall.

## Key Facts
- Miura 5 is an orbital recoverable small-lift launch vehicle developed by PLD Space (Spain).  
- Launch mass (launch weight): 69,025 kilograms (69025 kg).  
- Height: 35.7 metres.  
- Diameter: 2.0 metres.  
- Payload capacity: 1,080 kg to equatorial orbit.  
- Payload capacity: 540 kg to Sun-synchronous orbit.  
- Propulsion: five TEPREL-C sea-level engines and one TEPREL-C Vacuum engine.  
- Vehicle class: reusable launch vehicle, small-lift launch vehicle, two-stage-to-orbit.  
- Operator / manufacturer / designer: PLD Space.  
- Design lineage: follows Miura 1 and is part of the Miura family and the Future Launchers Preparatory Programme.  
- Designated start point (launch site): Guiana Space Centre.  
- Alias: Arion 2.  
- Official websites: https://pldspace.com/es/miura-5 (Spanish) and https://pldspace.com/en/miura-5 (English).

## FAQs
### Q: What is the payload capacity of Miura 5?
A: Miura 5 is rated to carry up to 1,080 kg to an equatorial orbit and up to 540 kg to a Sun-synchronous orbit.

### Q: Is Miura 5 reusable?
A: Yes. Miura 5 is classified as a reusable launch vehicle and is designed as a two-stage-to-orbit, recoverable rocket.

### Q: Who designs and operates Miura 5?
A: PLD Space is the designer, manufacturer, and operator of Miura 5.

### Q: What engines power Miura 5?
A: The vehicle uses five TEPREL-C engines (sea-level) on its first stage and one TEPREL-C Vacuum engine on its upper stage.

### Q: Where is Miura 5 intended to launch from?
A: The designated start point listed for Miura 5 is the Guiana Space Centre.

## Why It Matters
Miura 5 represents a European, Spanish-developed approach to the small-satellite launch market by combining recoverability with meaningful payload capability. As a recoverable, two-stage-to-orbit small-lift launcher, it targets missions that need dedicated access to low Earth orbits while enabling partial vehicle reuse to improve operations and cost-effectiveness. The vehicle’s payload margins (1,080 kg to equatorial orbit; 540 kg to Sun-synchronous orbit) position it to serve a range of commercial, scientific, and institutional small-satellite deployments. Being part of the Miura family and linked to the Future Launchers Preparatory Programme situates Miura 5 within broader European launcher development efforts. Its planned operations from the Guiana Space Centre provide an equatorial launch site option for customers. Overall, Miura 5 is notable for bringing a Spanish-built, reusable, small-lift orbital capability to the market, addressing demand for dedicated access to space for small payloads.

## Notable For
- Reusability: Classified as a recoverable/reusable small-lift launch vehicle in the Miura family.  
- Payload capability: Up to 1,080 kg to equatorial orbit and 540 kg to Sun-synchronous orbit.  
- Engine configuration: First stage powered by five TEPREL-C engines and upper stage by one TEPREL-C Vacuum engine.  
- Spanish design and manufacture: Developed, designed, and operated by Spanish company PLD Space.  
- Launch site designation: Identified start point is the Guiana Space Centre.

## Body

### Overview
- Miura 5 is an orbital, recoverable small-lift launch vehicle.  
- It is part of the Miura family of European launch vehicles developed by PLD Space.  
- The vehicle is an instance of a rocket model and is subclassed as a reusable launch vehicle, a small-lift launch vehicle, and a two-stage-to-orbit vehicle.

### Design and Configuration
- Two-stage-to-orbit architecture.  
- Recoverable/reusable design intent.  
- Follows the earlier vehicle Miura 1 in the Miura family.  
- Alias name: Arion 2.

### Dimensions and Mass
- Height: 35.7 metres.  
- Diameter: 2.0 metres.  
- Launch weight (mass): 69,025 kilograms.

### Performance and Payload
- Payload to equatorial orbit: 1,080 kilograms.  
- Payload to Sun-synchronous orbit: 540 kilograms.  
- Targeted at small-lift missions to low Earth orbit.

### Propulsion
- First stage propulsion uses five TEPREL-C engines.  
- Upper stage propulsion uses one TEPREL-C Vacuum engine.  
- Engine configuration supports staging and orbital insertion for small payloads.

### Launch and Operations
- Designated start point / launch site: Guiana Space Centre.  
- Operator and manufacturer: PLD Space.  
- Designed by PLD Space.

### Heritage and Program Links
- Part of the Miura family of launch vehicles.  
- Linked to the Future Launchers Preparatory Programme.  
- Follows Miura 1 in design lineage.

### Technical Specifications (selected)
- Launch mass: 69,025 kg (launch weight).  
- Height: 35.7 m.  
- Diameter: 2.0 m.  
- Engines: 5 × TEPREL-C (sea-level) + 1 × TEPREL-C Vacuum.  
- Payload: 1,080 kg (equatorial) / 540 kg (Sun-synchronous).  
- Country of origin: Spain.  
- Operator / Manufacturer / Designer: PLD Space.  
- Official pages: https://pldspace.com/es/miura-5 and https://pldspace.com/en/miura-5.

(Information in this entry is drawn from PLD Space specifications and the provided dataset.)

## References

1. [Source](https://pldspace.com/en/miura-5)