76 hot fire tests of the preburner, totaling some 400 seconds of test time, were executed from April–August 2015. [34] SpaceX plans to mass-produce up to 500 Raptor engines per year, each costing less than $250,000. If you had it at a high expansion ratio, has the potential to have a specific impulse of 380. Descente à l'horizontale du prototype SN9 de Starship en février dernier lors d'un vol d'essai. Cette déclaration a remis en cause une grande partie des spéculations autour de la configuration des moteurs qui voyaient majoritairement 9 moteurs sur le modèle des Falcon 9. [59][60], SpaceX successfully began development testing of injectors in 2014 and completed a full-power test of a full-scale oxygen preburner in 2015. [55] In April 2014, SpaceX completed the requisite upgrades and maintenance to the Stennis test stand to prepare for testing of Raptor components,[56] and the engine component testing program began in earnest, focusing on the development of robust startup and shutdown procedures, something that is typically quite difficult to do for full-flow staged combustion cycle engines. Toyota Hilux fans should be quite happy to hear of its new Mako package designed to shame the Ford Ranger Raptor back into extinction. Le 9 décembre 2020, le prototype du Starship SN8, équipé de trois moteurs raptor, effectue un vol à 12,5 km d'altitude. », « Musk said Lox and methane would be SpaceX’s propellants of choice on a mission to Mars, which has long been his stated goal. [29][57] A June 2014 talk by Mueller provided more specific engine performance target specifications indicating 6,900 kN (1,600,000 lbf) of sea-level thrust, 8,200 kN (1,800,000 lbf) of vacuum thrust, and a specific impulse (Isp) of 380 s (3,700 m/s) for a vacuum version. Six vacuum-optimized Raptor engines, providing 3,500 kN (790,000 lbf) of thrust each, would also be used on the ITS second stage, for a total of nine engines. [16][55] Initial testing was limited to components of the Raptor engine, since the 440 kN (100,000 lbf) test stands at the E-2 complex at Stennis were not large enough to test the full Raptor engine. Le moteur Raptor est alimenté par du méthane liquide et de l'oxygène liquide en utilisant un cycle à combustion étagée plus efficace[19]. Frederic L. 7 Fév. Tests continued at least into September 2015. While the optimized Raptor vacuum engine is aiming for an Isp of ~380 s (3,700 m/s),[100] the v1.0 Raptor vac design to support early Starship development has been made more conservative and is projecting an Isp of only 365–370 s (3,580–3,630 m/s), intentionally decreasing engine performance to obtain having test engines sooner. [87] On 3 April 2019, SpaceX conducted a successful static fire test, firing the engine for a few seconds while the vehicle remained tethered to the ground. [78], In the BFR update given in September 2018, Musk showed video of a 71-second hot fire test of a Raptor engine, and stated that "this is the Raptor engine that will power BFR, both the ship and the booster; it's the same engine. The Raptor engine has more than twice the thrust of SpaceX's Merlin engine that powers their current Falcon 9 and Falcon Heavy launch vehicles. La dernière modification de cette page a été faite le 1 avril 2021 à 20:56. The Raptor engine has gone through a number of design concepts for engine thrust, specific impulse, and sea-level-nozzle/vacuum-nozzle sizings, depending on the vehicle design concept SpaceX was working on at the time. Family of cryogenic methane-fueled rocket engines developed by SpaceX. En raison de la présence d'eau dans le sous-sol martien et de dioxyde de carbone dans l'atmosphère de la planète Mars, le méthane, qui est un hydrocarbure simple, peut être facilement synthétisé sur la planète rouge en utilisant la réaction de Sabatier[15]. Le moteur Raptor en développement tel que prévu en octobre 2013 au moment de l’équipement de la plateforme de Stennis était conçu pour générer plus de 2 940 kN de poussée dans le vide[3]. Le premier moteur Raptor pour le vide spatial (Vacuum -RVac) pour le Starship a été expédié de l'usine SpaceX de Hawthorne, en Californie, à McGregor, au Texas. [44], In November 2012, Musk announced a new direction for the propulsion division of SpaceX: developing methane-fueled rocket engines. The new package comes from Toyota's New Zealand division, which will produce the limited-run pickup inside its factory. Goal is <$250k for V2.0 is a 250 ton thrust-optimized engine, ie <$1000/ton", "Full year production is usually ~70% of peak daily rate, so 500/year. For reference, 330 bar on Raptor produces ~225 tons (half a million pounds) of force". [31], The Raptor engine uses a large number of coaxial swirl injectors[32] to admit propellants to the combustion chamber, rather than pintle injectors used on the previous Merlin rocket engines that SpaceX mass-produced for its Falcon family of launch vehicles. ", "SpaceX launches Starship SN15 rocket and sticks the landing in high-altitude test flight", "Musk unveils revised version of giant interplanetary launch system", "Completed a full duration test fire of the Raptor Vacuum engine at SpaceX's rocket development facility in McGregor, Texas", "Sea level Raptor's vacuum Isp is ~350 sec, but ~380 sec with larger vacuum-optimized nozzle", "V1.0 of Raptor Vac is suboptimal, as optimized for speed of development. Il équipe les étages inférieurs et supérieurs du lanceur super-lourd Starship construit par SpaceX. [102] Il indique en outre que le concept de moteur au nom de code Raptor sera maintenant basé sur la combustion de méthane. The vacuum version is targeting 840 metric tons of thrust with 380 sec. Ajouter au panier wishlist comparer. La production in-situ de ressources sur Mars a notamment été examinée par la NASA et jugée viable pour l'oxygène, l'eau et la production de méthane[16]. Il a publié aujourd'hui sur Twitter des images magnifiques et enflammées d'un tir d'essai du moteur Raptor. En juin 2014 Mueller a fourni plus de spécifications au cours d’une conférence. Ces engins spatiaux pourraient transporter à un prix abordable 100 tonnes de fret ou 100 personnes jusqu'à la surface de Mars. [98][22] By mid-2018, SpaceX was publicly stating that the sea-level flight version Raptor engine design, with a nozzle exit diameter of 1.3 m (4.3 ft), was expected to have 1,700 kN (380,000 lbf) thrust at sea level with an Isp of 330 s (3,200 m/s) increasing to an Isp of 356 s (3,490 m/s) in vacuum. Le projet Starship (BFR) de SpaceX progresse et vient de franchir une nouvelle étape avec le premier test statique d'allumage du moteur-fusée Raptor. Les moteurs en développement sont en italique. Le Raptor, le moteur de SpaceX utilisé pour alimenter le vaisseau spatial qui approche, a atteint de nouveaux degrés de puissance électrique tout au long de son développement. Les modifications apportées aux bancs d'essai par SpaceX font maintenant partie de l'infrastructure de test de Stennis et seront disponibles aux autres utilisateurs de l'installation après que SpaceX ait terminé son programme[3]. to serve the theoretical purpose of servicing an upper stage that could be used on the existing, Chantilly, Houston, Seattle, Washington DC, This page was last edited on 6 May 2021, at 20:50. The modifications to the test stands made by SpaceX are now a part of the Stennis test infrastructure and are available to other users of the test facility after the SpaceX facility lease was completed. Les moteurs ont été testées dans des conditions qui ressemblent à une démonstration de force: Both Merlin & Raptor could throttle way lower with added design complexity", "Raptor engine just reached 330 bar chamber pressure without exploding! [38][39][needs update], Initial development testing[37] of Raptor methane engine components was done at the Stennis Space Center in Hancock County, Mississippi, where SpaceX added equipment to the existing infrastructure in order to support liquid methane engine testing.
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