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P80 (stage)
The P80FW is a retired solid-fuel rocket motor developed as the first stage of the Vega launch vehicle. It was developed by Europropulsion, a joint venture between Avio and ArianeGroup, for the European Space Agency (ESA). The designation "P80FW" reflected key characteristics of the motor: "P" stood for ''poudre'' (French for 'powder'), referencing its solid propellant; "80" denoted the original target of 80 tonnes of propellant (later increased to 88 tonnes); and "FW" stood for ''filament wound'', indicating the one-piece carbon-fibre composite construction of the motor casing. Prior to its retirement, it was the world's most powerful monolithic solid rocket motor. History Development of the P80 began in 2005 led by the French space agency CNES, in collaboration with the ESA and the Italian Space Agency (ASI). The first static firing test was conducted at the Guiana Space Centre in November 2006, followed by qualification testing in December 2007. The P80 made its maiden fli ...
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Guiana Space Centre
The Guiana Space Centre (; CSG), also called Europe's Spaceport, is a spaceport to the northwest of Kourou in French Guiana, an Overseas departments and regions of France, overseas region of France in South America. Kourou is located approximately north of the equator at a latitude of 5°. In operation since 1968, it is a suitable location for a spaceport because of its near equatorial location and open sea to the east and north. At CSG, space launches are conducted by several European private companies and government agencies working together. The CSG land itself is managed by CNES, the French national space agency. The launch infrastructure built on the CSG land is owned by the European Space Agency. The private company Arianespace operates the launches including planning missions, handling customer relationships and overseeing the team at CSG that integrates and prepares vehicles for launch. The rockets themselves are designed and produced by other companies, ArianeGroup f ...
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Ariane 6
Ariane 6 is a European expendable launch system developed for the European Space Agency (ESA) and manufactured by a consortium of European companies, led by the prime contractor ArianeGroup. As part of the Ariane rocket family, it is operated by Arianespace, replacing the Ariane 5. The project's primary contributors were France (55.3%), Germany (21%) and Italy (7.6%), with the remaining work distributed among ten other participating countries. This two-stage rocket utilizes liquid hydrogen and liquid oxygen ( hydrolox) engines. The first stage features an upgraded Vulcain engine from Ariane 5, while the second uses the Vinci engine, designed specifically for this rocket. The Ariane 62 variant uses two P120C solid rocket boosters, while Ariane 64 uses four. The P120C booster is shared with Europe's other launch vehicle, and is an improved version of the P80 used on the original Vega. Selected in December 2014 over an all-solid-fuel alternative, Ariane 6 was initially ...
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Thrust Vector Control
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 vehicle. In rocketry and ballistic missiles that fly outside the atmosphere, aerodynamic control surfaces are ineffective, so thrust vectoring is the primary means of attitude control. Exhaust vanes and gimbaled engines were used in the 1930s by Robert Goddard. For aircraft, the method was originally envisaged to provide upward vertical thrust as a means to give aircraft vertical (VTOL) or short (STOL) takeoff and landing ability. Subsequently, it was realized that using vectored thrust in combat situations enabled aircraft to perform various maneuvers not available to conventional-engined planes. To perform turns, aircraft that use no thrust vectoring must rely on aerodynamic control surfaces only, such as ailerons or elevator; aircraft w ...
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SABCA
SABCA () is a Belgian aerospace company. Its main sectors of activity are civil aviation, space and defence. SABCA was established during 1920. Presently, it is owned by the Belgian group Orizio, itself owned by the Société Fédérale de Participations et d'Investissement (SFPIM) (a Belgian federal holding) and Sabena Aerospace. History During 1920, SABCA was founded with the purpose of locally designing and building aircraft to satisfy Belgium's emerging aviation requirements. Its first manufacturing site was adjacent to Haren Airport, in the suburbs of Brussels. During the Interwar period, the company produced a number of in-house designs, as well as engaging in the manufacture of both civil and military aircraft. Throughout its existence, SABCA has been a prolific user of production licenses, which have authorised the firm to build other manufacturers' aircraft. During 1926, the company constructed a total 15 Airco DH.4 light bombers.Jackson 1987, p. 60. While its opera ...
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Netherlands
, Terminology of the Low Countries, informally Holland, is a country in Northwestern Europe, with Caribbean Netherlands, overseas territories in the Caribbean. It is the largest of the four constituent countries of the Kingdom of the Netherlands. The Netherlands consists of Provinces of the Netherlands, twelve provinces; it borders Germany to the east and Belgium to the south, with a North Sea coastline to the north and west. It shares Maritime boundary, maritime borders with the United Kingdom, Germany, and Belgium. The official language is Dutch language, Dutch, with West Frisian language, West Frisian as a secondary official language in the province of Friesland. Dutch, English_language, English, and Papiamento are official in the Caribbean Netherlands, Caribbean territories. The people who are from the Netherlands is often referred to as Dutch people, Dutch Ethnicity, Ethnicity group, not to be confused by the language. ''Netherlands'' literally means "lower countries" i ...
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Specific Impulse
Specific impulse (usually abbreviated ) is a measure of how efficiently a reaction mass engine, such as a rocket engine, rocket using propellant or a jet engine using fuel, generates thrust. In general, this is a ratio of the ''Impulse (physics), impulse'', i.e. change in momentum, ''per mass'' of propellant. This is equivalent to "thrust per massflow". The resulting unit is equivalent to velocity. If the engine expels mass at a constant exhaust velocity v_e then the thrust will be \mathbf = v_e \frac . If we integrate over time to get the total change in momentum, and then divide by the mass, we see that the specific impulse is equal to the exhaust velocity v_e . In practice, the specific impulse is usually lower than the actual physical exhaust velocity inefficiencies in the rocket, and thus corresponds to an "effective" exhaust velocity. That is, the specific impulse I_ in units of velocity *is defined by* : \mathbf = I_ \frac , where \mathbf is the average thrust. ...
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Ariane 5
Ariane 5 is a retired European heavy-lift space launch vehicle operated by Arianespace for the European Space Agency (ESA). It was launched from the Guiana Space Centre (CSG) in French Guiana. It was used to deliver payloads into geostationary transfer orbit (GTO), low Earth orbit (LEO) or further into space. The launch vehicle had a streak of 82 consecutive successful launches between 9 April 2003 and 12 December 2017. Since 2014, Ariane 6, a direct successor system, first launched in 2024. The system was designed as an expendable launch vehicle by the ''Centre national d'études spatiales'' (CNES), the French government's space agency, in cooperation with various European partners. Despite not being a direct derivative of its predecessor launch vehicle program, it was classified as part of the Ariane rocket family. Aérospatiale, and later ArianeGroup, was the prime contractor for the manufacturing of the vehicles, leading a multi-country consortium of other European con ...
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Hydroxyl-terminated Polybutadiene
Hydroxyl-terminated polybutadiene (HTPB) is an oligomer of butadiene terminated at each end with a hydroxyl functional group. It reacts with isocyanates to form polyurethane polymers. HTPB is a translucent liquid with a color similar to wax paper and a viscosity similar to corn syrup. The properties vary because HTPB is a mixture rather than a pure compound, and it is manufactured to meet customers' specific requirements. A typical HTPB is R-45HTLO. This product consists of oligomeric units typically containing 40–50 butadiene molecules bonded together, with each end of the chain terminated with a hydroxyl Hgroup: R-45HTLO has a functionality of 2.4-2.6, which means that there is (approximately) one additional hydroxyl group located along the chain for every two oligomeric units. This provides side-to-side linkage for a stronger cured product. HTPB is usually cured by an addition reaction with di- or poly-isocyanate compounds. Uses Materials production Polyurethanes ...
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Aluminium Powder
Aluminium powder is powdered aluminium. This was originally produced by mechanical means using a stamp mill to create flakes. Subsequently, a process of spraying molten aluminium to create a powder of droplets was developed by E. J. Hall in the 1920s. The resulting powder might then be processed further in a ball mill to flatten it into flakes for use as a coating or pigment. Aluminium powder features low density with high conductivity. Characteristics Powdered aluminium shares many of the physical characteristics of bulk aluminium such as its molecular weight of 26.981538 g mol−1, melting point of 660 °C, and a boiling point of 2460 °C. It combusts at a much faster rate to bulk aluminium, this is due to the fact that the gaps between the particles allow for more air and therefor faster oxidization. Usage * autoclave aerated concrete * cosmetic colourant * fingerprint powder * metallic paint * pyrotechnics (including the M-80 firecracker) * refractory * r ...
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Ammonium Perchlorate Composite Propellant
Ammonium perchlorate composite propellant (APCP) is a solid rocket propellant. It differs from many traditional solid rocket propellants such as black powder or zinc-sulfur, not only in chemical composition and overall performance but also by being cast into shape, as opposed to powder pressing as with black powder. This provides manufacturing regularity and repeatability, which are necessary requirements for use in the aerospace industry. Uses Ammonium perchlorate composite propellant is typically for aerospace rocket propulsion where simplicity and reliability are desired and specific impulses (depending on the composition and operating pressure) of are adequate. Because of these performance attributes, APCP has been used in the Space Shuttle Solid Rocket Boosters, aircraft ejection seats, and specialty space exploration applications such as NASA's Mars Exploration Rover descent stage retrorockets. In addition, the high-power rocketry community regularly uses APCP i ...
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Vega E
VegaC, or Vega Consolidation, is a European expendable, small-lift launch vehicle developed and produced by Avio. It is an evolution of the original Vega launcher, designed to offer greater launch performance and flexibility. Approved for development by the European Space Agency (ESA) in December 2014, VegaC was designed to accommodate larger institutional payloads and compete effectively in the commercial launch market. Initially marketed and operated by Arianespace, the ESA decided in August 2024 to empower Avio to directly commercialize VegaC and seek non-governmental customers. This transition is anticipated to be complete by the end of 2025. VegaC, like its predecessor, is designed to launch small satellites for scientific and Earth observation missions to polar and sun-synchronous low Earth orbits. The reference VegaC mission places a spacecraft into a polar orbit, representing an or 60% increase over the original Vega. Named after Vega, the brightest star in the cons ...
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P160C
The P160C is a solid-fuel rocket motor developed for use as the first stage of the Vega C+ mid-life upgrade, the next-generation Vega E, and as strap-on boosters for the Ariane 6 Block 2 launch vehicles. It was developed by Europropulsion, a joint venture between Avio and ArianeGroup, for the European Space Agency (ESA). The designation "P160C" reflects key characteristics of the motor: "P" stands for ''poudre'' (French for 'powder'), referencing its solid propellant; "160" denoted the original target of 160 tonnes of propellant (later increased to 167 tonnes); and "C" signifies its ''common'' use across multiple launch systems. The motor was developed largely in response to the increased lift performance requirements of Project Kuiper, Amazon’s satellite internet constellation. Compared to its predecessor, the P120C, the P160C adds an additional of solid propellant and is taller. The motor's casing is constructed as a single-piece carbon-fibre composite shell, making it one ...
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