M10 (rocket Engine)
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M10 is a liquid-fuel
upper-stage A multistage rocket or step rocket is a launch vehicle that uses two or more rocket ''stages'', each of which contains its own engines and propellant. A ''tandem'' or ''serial'' stage is mounted on top of another stage; a ''parallel'' stage i ...
rocket engine A rocket engine uses stored rocket propellants as the reaction mass for forming a high-speed propulsive jet of fluid, usually high-temperature gas. Rocket engines are reaction engines, producing thrust by ejecting mass rearward, in accorda ...
by
Avio Avio S.p.A. is an Italian company operating in the aerospace sector with its head office in Colleferro near Rome, Italy. Founded in 1908, it is present in Italy and abroad with different commercial offices and 10 production sites. Avio operate ...
on behalf of
European Space Agency , owners = , headquarters = Paris, Île-de-France, France , coordinates = , spaceport = Guiana Space Centre , seal = File:ESA emblem seal.png , seal_size = 130px , image = Views in the Main Control Room (1205 ...
for use on Vega E. The engine, initially known as ''LM10-MIRA'', was a derivation of the existing Russian
RD-0146 The RD-0146 (РД-0146, Ракетный Двигатель-0146, Rocket Engine-0146) is a liquid-fuel cryogenic rocket engine developed by KBKhA Kosberg in Voronezh, Russia. The RD-0146 is the first Russian rocket engine to burn liquid oxyg ...
engine and result of a past collaboration between ''Avio'' and
Chemical Automatics Design Bureau Chemical Automatics Design Bureau (CADB), also KB Khimavtomatika (russian: Конструкторское бюро химавтоматики, КБХА, KBKhA), is a Russian design bureau founded by the NKAP (People's Commissariat of the Aircraf ...
(KBKhA) ended in 2014 after the escalation of the Russo-Ukrainian conflict and consequent
economic sanctions Economic sanctions are commercial and financial penalties applied by one or more countries against a targeted self-governing state, group, or individual. Economic sanctions are not necessarily imposed because of economic circumstances—they ma ...
. On May 6, 2022 engine testing campaign started at
Salto di Quirra Salto di Quirra is a restricted weapons testing range and rocket launching site near Perdasdefogu on Sardinia. It is the largest military range in Italy, composed of 12000 hectares of land owned by the Italian Ministry of Defence and one of the ...
,
Sardinia Sardinia ( ; it, Sardegna, label=Italian, Corsican and Tabarchino ; sc, Sardigna , sdc, Sardhigna; french: Sardaigne; sdn, Saldigna; ca, Sardenya, label=Algherese and Catalan) is the second-largest island in the Mediterranean Sea, after ...
, with consequent maiden flight on a Vega-E launcher expected by 2026 from
Guiana Space Centre The Guiana Space Centre (french: links=no, Centre spatial guyanais; CSG), also called Europe's Spaceport, is a European spaceport to the northwest of Kourou in French Guiana, a region of France in South America. Kourou is located approximatel ...
.


Overview

The M10 engine is the first operational European
methane Methane ( , ) is a chemical compound with the chemical formula (one carbon atom bonded to four hydrogen atoms). It is a group-14 hydride, the simplest alkane, and the main constituent of natural gas. The relative abundance of methane on Ea ...
rocket engine, conceived for use on upper stages of future ''Vega-E'' and ''Vega-E Light'' launchers, in which will replace both the solid-fueled Zefiro 3rd stage and hydrazine-fueled AVUM 4th upper stage. An industrial team directed by ''Avio'' with companies of
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,
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,
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,
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,
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and
Switzerland ). Swiss law does not designate a ''capital'' as such, but the federal parliament and government are installed in Bern, while other federal institutions, such as the federal courts, are in other cities (Bellinzona, Lausanne, Luzern, Neuchâtel ...
will manufacture the engine. The ''M10'' minimum thrust requirements are a thrust of with a propellant mixture ratio of 3.4 and a minimum specific impulse of 362s.


Development

A feasibility study on improving ''Vega'' started in 2004, when the rocket was still in development, with the aim of increase performance, reduce costs and move away from toxic hydrazine fuels. The study proposed a new three-stage version of the rocket named Lyra with a liquid oxygen-methane upper stage. In 2007
Avio Avio S.p.A. is an Italian company operating in the aerospace sector with its head office in Colleferro near Rome, Italy. Founded in 1908, it is present in Italy and abroad with different commercial offices and 10 production sites. Avio operate ...
and
KBKhA Chemical Automatics Design Bureau (CADB), also KB Khimavtomatika (russian: Конструкторское бюро химавтоматики, КБХА, KBKhA), is a Russian design bureau founded by the NKAP (People's Commissariat of the Aircraf ...
started the collaboration for the development of such an engine under an agreement signed between
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and
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governments in
Moscow Moscow ( , US chiefly ; rus, links=no, Москва, r=Moskva, p=mɐskˈva, a=Москва.ogg) is the capital and largest city of Russia. The city stands on the Moskva River in Central Russia, with a population estimated at 13.0 million ...
on November 28, 2000. The first phase of the collaboration, ended in 2008, aimed at designing a concept for a 10t thrust
LOx Liquid oxygen—abbreviated LOx, LOX or Lox in the aerospace, submarine and gas industries—is the liquid form of molecular oxygen. It was used as the oxidizer in the first liquid-fueled rocket invented in 1926 by Robert H. Goddard, an appli ...
- LNG engine. The second phase of the collaboration focused instead on designing, manufacturing and testing a 7.5t thrust ''LM10-MIRA'' demonstrator engine. The engine was successfully tested in June 2014 in
Voronezh Voronezh ( rus, links=no, Воро́неж, p=vɐˈronʲɪʂ}) is a city and the administrative centre of Voronezh Oblast in southwestern Russia straddling the Voronezh River, located from where it flows into the Don River. The city sits on the ...
,
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. After the end of the collaboration with ''KHBhA'', ''Avio'' continued the development of ''M10'' under the ''Vega-Evolution'' program returning to the original target thrust of 10t. Objectives were finalizing development of main subsystems such as
turbopumps A turbopump is a propellant pump with two main components: a rotodynamic pump and a driving gas turbine, usually both mounted on the same shaft, or sometimes geared together. They were initially developed in Germany in the early 1940s. The purpo ...
,
valves A valve is a device or natural object that regulates, directs or controls the flow of a fluid (gases, liquids, fluidized solids, or slurries) by opening, closing, or partially obstructing various passageways. Valves are technically fitting ...
,
igniter In pyrotechnics, a pyrotechnic initiator (also initiator or igniter) is a device containing a pyrotechnic composition used primarily to ignite other, more difficult-to-ignite materials, such as thermites, gas generators, and solid-fuel rockets. T ...
,
thrust vectoring Thrust vectoring, also known as thrust vector control (TVC), is the ability of an aircraft, rocket, or other vehicle to manipulate the direction of the thrust from its engine(s) or motor(s) to control the attitude or angular velocity of the ve ...
and a new ALM 3D printed Thrust Chamber Assembly (TCA). A subscale model of the TCA was tested successfully on 13 November 2018 in
Colleferro Colleferro (IPA: /kɔllefɛrro/) is a small town with 20 698 inhabitants of the Metropolitan City of Rome in the Lazio region of central Italy. It is a residential zone with many different industries and sports structures. It borders the City of F ...
, Italy. In February 2020 a full scale engine prototype with a 3D printed TCA was successfully tested at
NASA The National Aeronautics and Space Administration (NASA ) is an independent agency of the US federal government responsible for the civil space program, aeronautics research, and space research. NASA was established in 1958, succeeding t ...
Marshall Space Flight Center, firing 19 times for a total of 450 seconds. On May 6 2022, the engine test and qualification campaign started in Avio's new Space Propulsion Test Facility (SPTF) at the Salto di Quirra with a single firing of 20 seconds. The first series of testing concluded successfully in July 2022 with a total ignition time of more than 800 seconds.


See also

* Attitude Vernier Upper Module (AVUM) *
Prometheus (rocket engine) The Prometheus rocket engine is an ongoing European Space Agency (ESA) development effort begun in 2017 to create a reusable methane-fueled rocket engine for use on the Themis reusable rocket demonstrator and Ariane Next, the successor to Ariane 6 ...
*
Liquid rocket A liquid-propellant rocket or liquid rocket utilizes a rocket engine that uses liquid propellants. Liquids are desirable because they have a reasonably high density and high specific impulse (''I''sp). This allows the volume of the propellant ta ...
*
Vega (rocket) Vega ( it, Vettore Europeo di Generazione Avanzata, or french: Vecteur européen de génération avancée, or en, European Vector of Advanced Generation, meaning "Advanced generation European carrier rocket") is an expendable launch system in ...
*
RD-0146 The RD-0146 (РД-0146, Ракетный Двигатель-0146, Rocket Engine-0146) is a liquid-fuel cryogenic rocket engine developed by KBKhA Kosberg in Voronezh, Russia. The RD-0146 is the first Russian rocket engine to burn liquid oxyg ...


Comparable engines

* Aeon 1 * TQ-11


References

{{Rocket engines European Space Agency Rocket propulsion Rocket engines using methane propellant Rocket engines using the expander cycle