Function | Sub-orbital reusable launch vehicle |
---|---|
Manufacturer | PLD Space |
Country of origin | Spain |
Size | |
Height | 12.7 m (42 ft) |
Diameter | 0.7 m (2 ft 4 in) |
Mass | 2,550 kg (5,620 lb) |
Stages | 1 |
Capacity | |
Payload to suborbital (150 km) | |
Mass | 100 kg (220 lb) [1] |
Launch history | |
Status | Active |
Launch sites | El Arenosillo |
Total launches | 1 |
Success(es) | 1 |
Failure(s) | 0 |
Partial failure(s) | 0 |
First flight | October 7, 2023 |
First stage | |
Powered by | 1 TEPREL-B |
Maximum thrust | 30.2 kN (6,800 lbf) [2] |
Burn time | 122 seconds |
Propellant | liquid oxygen (1,000 L) / kerosene (600 L) [3] |
Miura 1 (previously called Arion 1) [4] [5] 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. [6] It was first launched successfully on October 7, 2023, at 00:19 UTC. [7] [8]
Miura 1 was originally proposed as a two-stage rocket capable of achieving suborbital flight. It was originally planned to be 12 m long, with a capacity of 250 kg (551 lb). The engines were to use liquid oxygen and kerosene as propellants. [9]
In its final design, Miura 1 is a 12.7 m long 0.7 m diameter one-stage rocket, propelled by one TEPREL-B engine. The vehicle can fly a payload of up to 200 kg on a suborbital trajectory. The propulsion system is equipped with actuators to tilt the engine for an active thrust vector control. [10] Additionally, Miura 1 is equipped with a recovery system using its engines and parachutes that enable PLD Space to recover the vehicle from the ocean and re-use the complete launch vehicle. [11] With this, it will be the first recoverable launch vehicle in Europe. [6] Miura 1 is intended to be used for scientific research or technology development in a microgravity environment and/or in the upper atmosphere. Furthermore, about 70% of the technology developed for Miura 1 is planned to be used on the Miura 5 orbital rocket. [12]
In December 2019 GMV announced that the Miura 1 avionics system had passed the qualification phase. [13]
In March 2020, the stress test of the Miura 1 pressurized tanks was carried out to check their ability to withstand the working pressure (more than 400 bars (5,800 psi)) with a successful result. [14] COPVs (Composite Overwrapped Pressure Vessel) are used to pressurize propellant tanks and are a fundamental element of many launchers. [15]
In July 2020 the German Center of Applied Space Technology and Microgravity (ZARM) successfully completed vibration tests of its payload that will fly on the first launch (Test Flight-1) of Miura 1. [16]
On April 7, 2022, the company carried out the first test of the complete launcher at its facilities in Teruel, being the first test in Europe of a rocket propelled by liquid fuel and aimed to reach space and developed by a private company. [17] [18] [19] [lower-alpha 1]
After the first launch, the company said that they developed Miura 1 for just under 30 million euros. [8]
The first test flight of Miura 1 was initially planned for 2021 [20] from an experimental rocket launch site in Almonte (Huelva), southwestern Spain, administered by El Arenosillo, [21] and it will carry a payload from the German Center of Applied Space Technology and Microgravity (ZARM). [5] Up to eight suborbital launches are targeted per year. It has been delayed to 2022. [22]
On May 31, 2023, Miura 1, a launch window opened at 00:00 UTC, but was cancelled due to upper-level winds. On June 17, the company tried again, but the ignition of the engines was cancelled due to the on-board systems detecting abnormal parameters in the vehicle. Following that, and taking into account the increased risk of fires around the launch area due to high temperatures, the company decided in coordination with the Civil Guard to postpone a new launch attempt until fall. [23] The launch occurred on October 7, 2023, at 00:19 UTC. [24] The rocket reached an apogee of 46 km. [7] PLD Space considers this first launch to have been a success despite the apogee being only 46 km instead of 80 km (the decision was made before the launch to target a low altitude, flatter trajectory instead of a high altitude trajectory because of range safety reasons). The rocket was unable to be recovered after it splashed down in the planned location in the Atlantic. After most probably developing a water leak into the fuel tank because of the rocket hitting the sea, the rocket sank. [8]
Space launch vehicle Volna, is a converted submarine-launched ballistic missile used for launching satellites into orbit. It is based on the R-29R designed by State Rocket Center Makayev and related to the Shtil' Launch Vehicle. The Volna is a 3-stage launch vehicle that uses liquid propellant. The warhead section is used for the payloads that can be either put into orbit with the help of an additional boost engine or travel along a sub-orbital trajectory to be recovered at the landing site. Volna can be launched from Delta III-class submarine or from land based facilities.
A launch vehicle is typically a rocket-powered vehicle designed to carry a payload from Earth's surface or lower atmosphere to outer space. The most common form is the ballistic missile-shaped multistage rocket, but the term is more general and also encompasses vehicles like the Space Shuttle. Most launch vehicles operate from a launch pad, supported by a launch control center and systems such as vehicle assembly and fueling. Launch vehicles are engineered with advanced aerodynamics and technologies, which contribute to high operating costs.
The INTA-255 was a Spanish sounding rocket developed by the Instituto Nacional de Tecnica Aerospacial.
The National Institute for Aerospace Technology "Esteban Terradas" is an autonomous agency of the Spanish public administration dependent on the Secretariat of State for Defence (SEDEF). It is responsible for the aerospace, aeronautics, hydrodynamics, and defense and security technologies research.
New Shepard is a fully reusable sub-orbital launch vehicle developed for space tourism by Blue Origin. The vehicle is named after Alan Shepard, who became the first American to travel into space and the fifth person to walk on the Moon. The vehicle is capable of vertical takeoff and landings. Additionally, it is also capable of carrying humans and customer payloads into a sub-orbital trajectory.
El Arenosillo Test Centre (CEDEA) is the name of a rocket launch site for suborbital rockets managed by INTA, located in Moguer (Spain). It is located in the province of Huelva, Andalucía, in the southwest coast of Spain (37.1° N, 6.7° W). CEDEA is adjacent to the Center of Excellence for Unmanned Systems (CEUS).
The XCOR Lynx was a proposed suborbital horizontal-takeoff, horizontal-landing (HTHL), rocket-powered spaceplane that was under development by the California-based company XCOR Aerospace to compete in the emerging suborbital spaceflight market. The Lynx was intended to carry one pilot, a ticketed passenger, and/or a payload above 100 kilometres (62 mi) altitude. The concept was under development since 2003, when a two-person suborbital spaceplane was announced under the name Xerus.
Tronador is a series of Argentine rockets, including the Tronador I and Tronador II vehicles, to develop a liquid-propellant rocket expendable launch system called ISCUL.
Capricornio was a Spanish satellite launch vehicle developed by the Instituto Nacional de Técnica Aeroespacial (INTA) in the 1990s. It was intended to be Spain's first launcher.
Electron is a two-stage, partially reusable orbital launch vehicle developed by Rocket Lab, an American aerospace company with a wholly owned New Zealand subsidiary. Electron services the commercial small satellite launch market. It's the third most launched small-lift launch vehicle in history. Its Rutherford engines are the first electric-pump-fed engine to power an orbital-class rocket. Electron is often flown with a kickstage or Rocket Lab's Photon spacecraft. Although the rocket was designed to be expendable, Rocket Lab has recovered the first stage twice and is working towards the capability of reusing the booster. The Flight 26 (F26) booster has featured the first helicopter catch recovery attempt. Rocket Lab has, however, abandoned the idea of catching Electron.
Zero 2 Infinity is a private Spanish company developing high-altitude balloons intended to provide access to near space and low Earth orbit using a balloon-borne pod and a balloon-borne launcher.
Exos Aerospace Systems & Technologies is an aerospace manufacturer and developer of reusable launch systems intended to support uncrewed orbital spaceflight launches, and is based in Caddo Mills, Texas.
Payload Aerospace S.L. is a Spanish company developing two partially-reusable launch vehicles called Miura 1 and Miura 5.
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.
El Hierro Launch Centre is a proposed project by Instituto Nacional de Técnica Aeroespacial (INTA) to create a spaceport on the island of El Hierro, part of the Canary Islands. It would be located in the south of the island, in the area of Tacorón, 5 km from La Restinga. in the municipality of El Pinar, Canary Islands. It is being proposed as a center of civil use exclusively, for the launch of micro- and nanosatellites with scientific or commercial objectives, such as telecommunications or Earth observation.
The INTA-100 vehicle was a small 2-stage meteorological sounding rocket designed and developed between the 1980s and the 1990s by the Instituto Nacional de Técnica Aeroespacial (INTA). The final design was entirely produced in Spain to be used by the Instituto Nacional de Meteorología in conducting experiments on the atmosphere.
TEPREL is a family of rocket engines designed and built by the Spanish aerospace company PLD Space for their Miura 1 and Miura 5 launch vehicles. The TEPREL engine, named after the Spanish reusable engine program that is financing its development, uses kerosene and liquid oxygen as propellants. So far, several versions of this engine, intended to propel Miura 1, have been developed and tested on the company's own liquid propulsion test facilities located in Teruel, Spain.
BluShift Aerospace is an employee-owned American aerospace firm based in Brunswick, Maine. Targeting the growing smallsat and cubesat launch markets, bluShift is developing suborbital sounding rockets and small-lift orbital rockets which will be launched from a proposed new spaceport in Maine. The company has received primary funding from NASAs SBIR grant program, the National Science Foundations I-Corps grant program, the Maine Technology Institute, and the Maine Space Grant Consortium. The company has active operations at the former Brunswick Naval Air Station and Loring Air Force Base.