Function | partially reusable orbital launch vehicle |
---|---|
Manufacturer | PLD Space |
Country of origin | Spain |
Size | |
Height | 60 m (200 ft) [1] |
Diameter | 3.5 m (11 ft) [1] |
Stages | 2 |
Capacity | |
Payload to Low Earth orbit (LEO) | |
Mass | 13,580 kg (29,940 lb) [1] |
Payload to SSO | |
Mass | 11,275 kg (24,855 lb) [1] |
Payload to GTO | |
Mass | 4,595 kg (10,130 lb) [1] |
Launch history | |
Status | Under development |
Launch sites | Guiana Space Centre (planned) |
First flight | Planned for 2030 |
First stage | |
Diameter | 3.5 m (11 ft) |
Powered by | 5 |
Maximum thrust | 5,530 kN (1,240,000 lbf) |
Propellant | LOX / RP-1 |
Second stage | |
Powered by | 1 |
Propellant | LOX / RP-1 |
The Miura Next is a future reusable heavy-lift rocket currently in development,part of PLD Space's program for the next 20 years. Designed to compete in the market of reusable launchers,it will allow for the transport of large payloads to low Earth orbits and beyond. With capabilities for crewed missions and reusable first stages,it aims to position itself as a European alternative to rockets like the Falcon 9. It is expected to work alongside the crewed capsule Lince,expanding the capabilities for space exploration and commercial ventures. [2]
The rocket was introduced by PLD Space in October 2024 as part of their space program for the next two decades. The company,headquartered in Elche,Spain,revealed their new reusable heavy-lift rocket during an event that showcased their commitment to innovation and competitiveness in the global launch market,targeting the first half of the 2030s for its maiden flight. [3]
Both the rocket and the crewed capsule Lince were developed in secrecy by the company until their development was made public during an event marking the anniversary of the first launch of Miura 1, [4] which was expected to provide updates on the development of the Miura 5. [5]
The Miura Next will be a reusable rocket that is part of PLD Space's new family of launchers. Versions currently named Miura Next Heavy and Super Heavy will be able to place up to 53 tons into low Earth orbit. Additionally,they will be capable of carrying between 2.4 and 16 tons to the Moon and Mars,depending on their configuration,which may include up to four booster engines that will also be reusable. [6]
The first flight is expected in 2030,and by 2035,it is projected to be one of the most powerful rockets in the world,with scalable and reusable technology. It will also be the only one of its kind within the European Union,as the company aims to establish independence for the EU in terms of space travel. [7]
The following table lists the expected payload capabilities for the various vehicle configurations to different destinations.
Destination | Miura Next | Miura Next Heavy | Miura Next Super Heavy | |||
---|---|---|---|---|---|---|
Expendable | Reusable (barge) | Reusable (return to launch site) | Expendable | Reusable [a] | Expendable | |
LEO (420 km) | 13,580 kg | 10,200 kg | 6,650 kg | 36,000 kg | 19,500 kg | 53,000 kg |
SSO (500 km) | 11,275 kg | 8,300 kg | 5,130 kg | 30,580 kg | 16,250 kg | – |
GTO | 4,595 kg | 2,900 kg | 1,100 kg | 15,140 kg | 7,160 kg | 23,000 kg |
Moon | – | – | – | – | – | 16,695 kg |
Mars | – | – | – | – | – | 13,660 kg |
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A booster is a rocket used either in the first stage of a multistage launch vehicle or in parallel with longer-burning sustainer rockets to augment the space vehicle's takeoff thrust and payload capability. Boosters are traditionally necessary to launch spacecraft into low Earth orbit, and are especially important for a space vehicle to go beyond Earth orbit. The booster is dropped to fall back to Earth once its fuel is expended, a point known as booster engine cut-off (BECO).
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The Exploration Systems Architecture Study (ESAS) is the official title of a large-scale, system level study released by the National Aeronautics and Space Administration (NASA) in November 2005 of his goal of returning astronauts to the Moon and eventually Mars—known as the Vision for Space Exploration. The Constellation Program was cancelled in 2010 by the Obama Administration and replaced with the Space Launch System, later renamed as the Artemis Program in 2017 under the Trump Administration.
Long March 5, or Changzheng 5 (CZ-5), and also by its nickname "Pang-Wu", is a Chinese heavy-lift launch vehicle developed by the China Academy of Launch Vehicle Technology (CALT). It is the first Chinese launch vehicle designed to use exclusively non-hypergolic liquid propellants. It is the fifth iteration of the Long March rocket family.
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The Ares V was the planned cargo launch component of the cancelled NASA Constellation program, which was to have replaced the Space Shuttle after its retirement in 2011. Ares V was also planned to carry supplies for a human presence on Mars. Ares V and the smaller Ares I were named after Ares, the Greek god of war.
Falcon Heavy is a super heavy-lift launch vehicle with partial reusability that can carry cargo into Earth orbit, and beyond. It is designed, manufactured and launched by American aerospace company SpaceX.
SpaceX manufactures launch vehicles to operate its launch provider services and to execute its various exploration goals. SpaceX currently manufactures and operates the Falcon 9 Block 5 family of medium-lift launch vehicles and the Falcon Heavy family of heavy-lift launch vehicles – both of which are powered by SpaceX Merlin engines and employ VTVL technologies to reuse the first stage. As of 2024, the company is also developing the fully reusable Starship launch system.
SpaceX has privately funded the development of orbital launch systems that can be reused many times, similar to the reusability of aircraft. SpaceX has developed technologies over the last decade to facilitate full and rapid reuse of space launch vehicles. The project's long-term objectives include returning a launch vehicle first stage to the launch site within minutes and to return a second stage to the launch pad, following orbital realignment with the launch site and atmospheric reentry in up to 24 hours. SpaceX's long term goal would have been reusability of both stages of their orbital launch vehicle, and the first stage would be designed to allow reuse a few hours after return. Development of reusable second stages for Falcon 9 was later abandoned in favor of developing Starship, however, SpaceX developed reusable payload fairings for the Falcon 9.
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Payload Aerospace S.L. is a Spanish company developing two partially-reusable launch vehicles called Miura 1 and Miura 5.
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Miura 1 is a suborbital recoverable launch vehicle developed by the Spanish company PLD Space. It is the first launch vehicle in Europe that is designed to be recoverable. It was first launched successfully on October 7, 2023, at 00:19 UTC.
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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.
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