The engine was never used, and for many years it was at the Smithsonian Institution. The cookie is used to store the user consent for the cookies in the category "Analytics". By 1959, Rocketdyne built an uncooled boilerplate engine and achieved short-duration but stable 1M lbT, but it was prone to rough starts and destructive combustion instability. Although Rocketdyne solved the LOX pump problem, the people familiar with the engine would cringe when 110 seconds went by and, then, breathe again. [28] The recovered parts were brought to the Kansas Cosmosphere and Space Center in Hutchinson for the process of conservation. LOX pump failures resulted in explosive fires that converted failed components into ions. These cookies help provide information on metrics the number of visitors, bounce rate, traffic source, etc. Part 8.11: The Rocketdyne F-1 Engine Engineers scrutinized the LOX pump seals and bearings, but the failures persisted. The F-1 turbopump was a marked departure from the tried and true Mark 3 turbopump that had served Atlas, Thor, Jupiter and the H-1. Functional cookies help to perform certain functionalities like sharing the content of the website on social media platforms, collect feedbacks, and other third-party features. To subscribe to this RSS feed, copy and paste this URL into your RSS reader. In 2013, engineers at the Marshall Space Flight Center began tests with an original F-1, serial number F-6049, which was removed from Apollo 11 due to a glitch. The F-1 was a liquid-fueled rocket motor, burning RP-1 (kerosene) as fuel, and using liquid oxygen (LOX) as the oxidizer. According to F-1 engineer Robert Biggs, "A combustion disturbance occurred with unprecedented ferocity." Plaque at the memorial and observations. Especially the potential use of RL10 on the evolved upper stage, that would've taken SpaceX down a very different development path. The turbopump also presented development challenges. Silverstein insisted that the F-1 should produce 1.5M lbT, same as the total thrust of the Saturn IB. I know it's not that important when it comes to the usefulness of the rocket, but it's one of those numbers that can impress car guys, and really put the power inter perspective. Two incidents were traced to structural failures of the LOX pump impeller, which called for redesign of the unit with increased strength. Barber-Nichols (BN) entered the space launch industry in 1996, and since that time developed Rocket Engine Turbopumps for NASA, the U.S. Military, and private industry. This website depends on cookies to make it function. Rocketdyne presented the results of this study to the Air Force in 1957 and the Air Force told Rocketdyne to go build one. This was no easy task and there were some spectacular failures along the way, but by the time the Saturn V flew, F-1 engine performance was nearly flawless. Despite the F-1's dumbness, it operated at an unprecedented 1,125 psia chamber pressure, which resulted in many new details that had to be refined and many problems that had to be overcome. You also have the option to opt-out of these cookies. The first F-1 was delivered to NASA MSFC in October 1963. The F-1 engine is the most powerful single-nozzle liquid-fueled rocket engine ever flown. Of course this will not happen for sure, but it is still interesting to think about. On May 20, 2017 the Apollo permanent exhibit opened at the Museum of Flight in Seattle, WA and displays engine artifacts recovered including the thrust chamber and thrust chamber injector of the number 3 engine from the Apollo 12 mission, as well as a gas generator from an engine that powered the Apollo 16 flight. Other uncategorized cookies are those that are being analyzed and have not been classified into a category as yet. Environmentally, the turbopump was required to withstand temperatures ranging from input gas at 1,500F (820C) to liquid oxygen at 300F (184C). the fuel output was routed elsewhere or whether the fuel turbopump was run dry Published 13 May 2021; Revised 7 Dec 2022. Flight engines never got up above 800 sec. The fuel pump produced 15,471 gallons (58,564 litres) of RP-1 per minute while the oxidizer pump delivered 24,811 gal (93,920 l) of liquid oxygen per minute. Hot gases for the turbopump turbine originated in the gas generator and entered the turbine at 77 kilograms per second.47 A series of failures, 11 in all, dogged the development of the turbopumps for the F-1 engine. It does not store any personal data. In this one second, from this single engine, 34 million BTUs of energy have been released, enough to raise the temperature of an Olympic sized swimming pool 6.2 F. This includes design, procurement, manufacturing, and test support from development to flight units all under one roof. It was intended for Falcon 1. F 1 Rocket Engine Horsepower formulaf1results.blogspot.com. Eventually, engine combustion was so stable, it would self-damp artificially induced instability within one-tenth of a second. He stated that the design of the rocket engine hinged on the question of whether the pump design was viable. The video does cover all of the essential parts of how a rocket turbopump works and what technical challenges engineers face when trying to make the more powerful ones like SpaceX is making. Two incidents were traced to structural failures of the LOX pump impeller, which called for redesign of the unit with increased strength. SA-500D, the Dynamic Test Vehicle, is on display at the U.S. Space and Rocket Center in Huntsville, Alabama. Clearly, extensive development was going to be required. Environmentally, the turbopump was required to withstand temperatures ranging from input gas at 1,500 F (816 C), to liquid oxygen at 300 F (184 C). https://www.youtube.com/watch?v=1AD-DbC3e68, https://www.quora.com/What-was-the-horsepower-and-torque-of-the-Saturn-V-rocket, Rocketdyne-developed rocket engine used for Saturn V, SpaceX Falcon 1 (obsolete medium-lift vehicle), Interplanetary Transport System (2016 oversized edition) (see MCT), Merlin 1 kerolox rocket engine, revision C (2008), 556-660kN, Portmanteau: liquid hydrogen/liquid oxygen mixture, Portmanteau: kerosene/liquid oxygen mixture, Portmanteau: methane/liquid oxygen mixture, High-pressure turbine-driven propellant pump connected to a rocket combustion chamber; raises chamber pressure, and thrust. [13][14] Due to the engine's potential advantage in specific impulse, if this F-1B configuration (using four F-1Bs in total) were integrated with the SLS Block 2, the vehicle could deliver 150 tonnes (330,000lb) to low Earth orbit,[15] while 113 tonnes (249,000lb) is what is regarded as achievable with the planned solid boosters combined with a four-engine RS-25 core stage. The liquid fueled Rocketdyne F-1 engine, installed in quintiplicate for the mighty Saturn V rocket's S-IC first stage, powered mankind to the Moon in the late 1960s. Also, note that the target chamber pressure for this engine was 890psi. With the proper welding requirements finally established, Rocketdyne adopted an automatic welding procedure to complete the "fix" on this situation.48. The reduction in parts costs is aided by using selective laser melting in the production of some metallic parts. Using a Counter to Select Range, Delete, and Shift Row Up, Indefinite article before noun starting with "the", How to make chocolate safe for Keidran? F1 Rocket and F4 Raider NEWS; Team Rocket Newsletters; FAQs, Specs, and related Rocket Links Engine used: Lycoming IO-540: HP Range: 250-300: Fuel Capacity: 42 to 52 gal: Empty Weight: 1200lbs: Gross Weight: 2000 lbs: +6 and -3 g: Home of the F1 Rocket and F4 Raider I'm interested in JUST the fuel pump. Following these dictates, Rocketdyne followed the S-3D and H-1 proven examples in propellant choice (RP-1 and LOX), overall packaging, thrust chamber design, gas generator cycle, pressure ladder start sequence and using a heat exchanger to vaporize LOX and heat helium to pressurize the LOX and RP-1 tanks. In the case of the M-1, the hydrogen and oxygen turbopumps were completely separate, each using their own turbine, rather than running both off a common power shaft. [4]. Since 1966, BN specialized in the design and production of innovative turbomachinery, the use of advanced materials, and Design for Manufacturability. my September 2013 visit, it was still sitting upright near the former location of A domed chamber at the top of the engine served as a manifold supplying liquid oxygen to the injectors, and also served as a mount for the gimbal bearing which transmitted the thrust to the body of the rocket. This engine was It was installed in 1979, and moved from the parking lot across the street some time after 1980.[22]. A turbopump was used to inject fuel and oxygen into the combustion chamber. The cleaning procedure involved pumping TCE through the engine's fuel system and letting the solvent overflow for a period ranging from several seconds to 3035 minutes, depending upon the engine and the severity of the deposits. Bezos plans to put the engines on display at various places, including the National Air and Space Museum in Washington, D.C.[27]. The F-1 design initially specified a 1,125 psi chamber pressure at a time when the only 520 psi had been successfully achieved. Rocketdyne built 98 production F-1s, 70 of which were tested in S-ICs. Acceptance testing took a total of 495 sec, for a mission duration of 165 sec. The engine finally reached its full duration rated thrust on 26 May 1962. The turbopump on the F1 was considered part of the engine, but the turbopump didnt depend on the main part of the engine in order to run. Finally, on 18 Nov 1963, an engine under test at MSFC failed but did not catch fire. The first stage of the Saturn V had five F-1's for a total lift-off thrust of 7.5 million pounds. Rocket engine used on the Saturn V rocket, Doherty, Kerry (November 2009). The F-1's 2,500 pound turbopump pumped in the propellants at 42,500 gallons per minute. --- One Second in the Life of the Rocketdyne F-1 Rocket Engine, by Tom Fey ---. The Project Go team led a huge two-year effort to understand combustion instability and improve the injector. The F-1 is the largest, highest-thrust single-chamber, single-nozzle liquid-fuel engine flown. [12], In 2012, Pratt & Whitney, Rocketdyne, and Dynetics, Inc. presented a competitor known as Pyrios, a liquid rocket booster, in NASA's Advanced Booster Program, which aims to find a more powerful successor to the five-segment Space Shuttle Solid Rocket Boosters intended for early versions of the Space Launch System. The turbine was driven at 5,500 RPM by the gas generator, producing 55,000 brake horsepower (41 MW). Chamber pressure of the F1 on SaturnV was 1015psi and the chamber pressure for the upcoming Raptor engine is 4351psi (300 bar). The heaviest lifting is complete; the mission now depends on thrust from the upper stages to succeed. The fuel is also used to lubricate by splash and spray the three main bearings of the turbopump at 200 to 540 psig before entering the injector plate at 375 psig. The three cores produced a total of 80.5 million hp. The spent preburner exhaust is directed outside of the main throat and bell as exhaust. Source: https://www.enginehistory.org/Rockets/RPE08.11/RPE08.11.shtml. This engine uses a gas-generator cycle developed in the United States in the late 1950s and was used in the Saturn V rocket in the 1960s and early 1970s. It takes 3.2 million BTU per second to generate the 55,000 horsepower, enough power to lift a diesel locomotive 70 feet into the air in one second. https://www.nasa.gov/centers/marshall/history/f1_engine_new.html The rocket engine turbopump, in addition to being a high energy/weight ratio machine, must be designed to operate with the pump at cryogenic conditions and the turbine at high temperature. This requires design concepts that provide thermal growth flexibility while reacting large torques, separating loads and external ducting loads. NSF and SpaceX reach agreement on astronomy, but IDA sues Press J to jump to the feed. Below the thrust chamber was the nozzle extension, roughly half the length of the engine. The F-1 used RP-1, a type of kerosene, and liquid oxygen as the propellants. This cookie is set by GDPR Cookie Consent plugin. Elon tweets they're planning "about five full stacks" Boca Chica residents have been asked to be away all day Falcon Heavy | USSF-67 | A launch infographic. It should be 41 MW. To get the best experience possible, please download a compatible browser. The Comet HLLV would have used five F-1A engines on the main core and two on each of the boosters.[11]. The Merlin Engine produces more than 100,000 pounds of thrust at sea level and the turbopump is the lightest in its thrust class. Each F-1 was tested individually for a 40-sec calibration run and a 165-sec mission duration test. https://history.nasa.gov/SP-4206/ch4.htm If you could slow time and examine what happened during one of those magnificent operational seconds, what would you find? Merlin 1B was canceled from flight use before Falcon 5 was canceled. [28][27], In August 2014, it was revealed that parts of two different F-1 engines were recovered, one from Apollo 11 and one from another Apollo flight, while a photograph of a cleaned-up engine was released. The hydrogen and oxygen pumps were some of the most powerful ever built at the time, producing 75,000 horsepower for the former, and 27,000 hp (20,000 kW) for the latter. Five F-1 engines were used in the S-IC first stage of each Saturn V, which served as the main launch vehicle of the Apollo program. Another ten engines were installed on two ground test Saturn Vs never intended to fly. When work on the F-1 began, the most powerful production rocket engine produced around 150,000 lbT. Barber-Nichols (BN) has successfully developed the Propellant turbopumps for Virgin Orbits LauncherOne booster and upper stage liquid (If It Is At All Possible). For some reason the number 14,000 is rattling around in my head, but I have no sources. [needs update], Sixty-five F-1 engines were launched aboard thirteen Saturn Vs, and each first stage landed in the Atlantic Ocean. The F-1's problems now became front and center since there was no "plan B" for getting to the moon without the F-1. The F-1 remai Oxygen-rich, Closed-Cycle, Staged-Combustion Engine This engine was constructed in 1963 by the Rocketdyne Division of Rockwell International and underwent four start tests, totaling 192.6 seconds. We use cookies to optimize our website. turbopump saturn rocketdyne jupiter combustion. inspection of the "injector" and of the aft face of the second stage turbine Designer of the pump for the E-1/F-1 for Rocketdyne was Ernest A. Lamont. Necessary cookies are absolutely essential for the website to function properly. The source contains a small math error there. Each F-1 engine had more thrust than three Space Shuttle Main Engines combined. Seeing that jet of water that could easily fly over my house with such a wimpy pump being fueled with just Hydrogen Peroxide, it should give you at least a sense of scale for just how much liquid those pumps can move. In this one second, 413.5 gallons of liquid oxygen at -297 F, equivalent in volume to a six-horse pole barn filled with pure oxygen at 14.7 psi, and 258 gallons of RP-1 rocket grade kerosene fuel, roughly equivalent to a long-haul semi-trailer tractor's fuel capacity, have been supplied to the injector plate at the top of the engine. Expertise in these disciplines positioned Barber-Nichols to become one of the worlds leading developers of Rocket Engine Turbopump technology. This scheme actually did get tested but was replaced as soon as it was practical. On March 28, 2012, a team funded by Jeff Bezos, founder of Amazon.com, reported that they had located the F-1 rocket engines from an Apollo mission using sonar equipment. Methane would also be able to provide pressurisation for fuel and LOX could be pressurised with GOX, so basically methane would mostly replace helium. southeast of the S-IC Test Stand (Google All three pumps had their own lubrication system. For over 20 years, BN has designed and built more new rocket engine turbopumps than any other company in the United States. What are the issues and concerns related to turbopump blade cracks and manned spaceflight? MathJax reference. The engine is on loan to the museum from the Smithsonian's National Air and Space Museum. Also crazy to know that Madsen is now awaiting trial for murdering a reporter on his submarine. In essence, Breviks job was to make sure it doesnt melt. Through Breviks calculations of the hydrodynamic and thermodynamic characteristics of the F-1, he and his team were able to fix an issue known as starvation. The cluster of five F-1 engines burned a mixture of liquid oxygen and kerosene fuel at more than 15 metric tons per second during its two-and-one-half-minutes of operation. Each F-1 engine had more thrust than three space shuttle main engines combined to lift the vehicle to a height of about 36 miles and to a speed of about 6,000 mph. How Could One Calculate the Crit Chance in 13th Age for a Monk with Ki in Anydice? Was just thinking, how interesting and cool it would be developing a methalox-driven turbopump for Merlin. Well, I'm glad they seem to have found the error soon enough. [7][8] The F-1 rocket engine had its LOX dome, gas generator, and thrust chamber fuel jacket flushed with TCE during launch preparations.[8]. Issued by Microsoft's ASP.NET Application, this cookie stores session data during a user's website visit. How do I submit an offer to buy an expired domain? The designers could then quickly experiment with different co-axial fuel-injector designs to obtain the one most resistant to instability. Barber-Nichols used its experience gained on the Fastrac and Bantam projects to rapidly develop the Merlin Turbopump. Press question mark to learn the rest of the keyboard shortcuts. I Actually Believe Theyll Hit This Timeline, Elon on Twitter: "Starship launch attempt soon", Its Official, WDR is Going Down Tomorrow, Amazing photo of Falcon heavy clearing the TE. Since turbopump horsepower is tied closely to chamber pressure and mass flow rate, there is a good chance that Raptor may surpass the F1 turbopump horsepower (depending on mass flow rate of the Raptor). Structurally, fuel was used to lubricate and cool the turbine bearings. The Saturn V could have never achieved its objective of sending humans to Earths moon were it not for the F-1 engine. If you continue to browse, scroll, click or otherwise interact, you are providing implicit acknowledgement of and agreement to this. The first design featured three turbopumps. Robert Biggs, who in November 1967 was at the window in Firing Room 2, three miles away from the first Saturn V launch, commented, "I considered that the highpoint of my career. Create an account to follow your favorite communities and start taking part in conversations. It is the only F-1 on display outside the United States. with questions or comments about this web site. But hey, when, did unit conversion ever cause any problems, https://www.enginehistory.org/Rockets/RPE08.11/RPE08.11.shtml, Microsoft Azure joins Collectives on Stack Overflow. [3] Initially, progress on this problem was slow, as it was intermittent and unpredictable. Early development tests revealed serious combustion instability problems which sometimes caused catastrophic failure. At a point when it was a major engineering accomplishment to increase engine thrust by only 10%, the idea of increasing the thrust of a single engine by a factor of 10 was absurd. It was then collected by the bottom torus, which was connected to the upper one by four large trombone tubes, each of which included a fuel valve. Part 8.21: The Pratt & Whitney RL10 Engine, Part 9.10: The Apollo Launch Escape System, Part 9.20: The Apollo Command Module (CM), Part 9.21: Apollo CM Guidance and Navigation, Part 9.41: The LM Descent Propulsion System, Part 9.43: The LM Ascent Propusion System, Part 9.45: The LM Reaction Control System, Oefelein, Joseph C. and Vigor Yang "Comprehensive Review of Liquid-Propellant Combustion Instabilities in F-1 Engines", One Second in the Life of the Rocketdyne F-1 Rocket Engine. This engine uses a gas-generator cycle developed in the United States in the late 1950s and was used in the Saturn V rocket in the 1960s and early 1970s. The new pump also had dual symmetrical outlets on both the fuel and LOX pumps; this divided the total head rise load by two and reduced the duct and valve sizes. The combined flow rate of the five F-1s in the Saturn V was 3,357USgal (12,710L)[5] or 28,415lb (12,890kg) per second. Cold Cal. Explosions occurred in the other nine instances, with five during engine tests and four during component tests of the turbopump. YSC cookie is set by Youtube and is used to track the views of embedded videos on Youtube pages. https://www.enginehistory.org/Rockets/RPE08.11/RPE08.11.shtml A simple concept with an incredibly complicated execution that lasted only 2.7 minutes, the Rocketdyne F-1 engine has performed an epic, Herculean feat rewarded with a successful Apollo exit from Mother Earth and a glorious Viking death. Test firings of F-1 components had been performed as early as 1957. Below this dome were the injectors, which directed fuel and oxidizer into the thrust chamber in a way designed to promote mixing and combustion. F1 Rocket and F4 Raider news, specs, and misc. They were damaging after approximately 110 seconds of operation" come from? The F-1 engine - the most The Bantam Turbopump and the Fastrac Turbopump are two examples that demonstrate the cutting-edge turbopump expertise available at Barber-Nichols. While the production F-1 was a very simple engine, its initial design was quite complex. The turbine was driven at 5,500 RPM, producing 55,000 brake horsepower (41MW). The cookie stores information anonymously and assigns a randomly generated number to recognize unique visitors. [Thread #860 for this sub, first seen 2nd Mar 2018, 02:24] ^[FAQ] [Full ^list] ^[Contact] [Source ^code]. The test engine was fitted with a special rough combustion sensor that shut it down with little of no damage if instability was detected. Working much like a human heart, a rockets turbopump is a complex engine component that pumps fuel into an engine. Christian Science Monitor: a socially acceptable source among conservative Christians? In algorithms for matrix multiplication (eg Strassen), why do we say n is equal to the number of rows and not the number of elements in both matrices? The F-1 produced 1.5 million pounds of thrust. But on 28 Jun 1962 disaster struck. F1 Rocket Engine Thank you very much for downloading F1 Rocket Engine. If you continue to browse, scroll, click or otherwise interact, you are providing implicit acknowledgement of and agreement to this. If you (or anybody else) want to see some information about a turbopump on a more human scale, this video by Copenhagen Suborbitals shows you how they built one of their turbopumps that they used on a very early prototype rocket that only went suborbital: https://www.youtube.com/watch?v=p6BC1QfA0Ug. In this one second, the rotor of the dual-function MK-10 centrifugal turbopump, the size of a commercial refrigerator, weighing 2,500 lb, and powered by an impulse gas turbine generating 55,000 horsepower, has spun 91.5 times. It was the 25th out of 114 research and development engines built by Rocketdyne and it was fired 35 times. Your browser or your browser's settings are not supported. The combined propellant flow rate of the five F-1s in the Saturn V was 3,357 US gallons (12,710 l) per second. The turbopump upgrades were handled by Barber-Nichols, Inc. for SpaceX. (which would seem to alter the performance of the turbopump). This power level is equivalent to more than 120 automobiles, or 90 light aircraft, or even 5 diesel-electric locomotives. Now that is fuel rich combustion. Right, but that's the power of the total rocket power, right? The first unit was delivered to the customer less than one year after design work began. A variation of the _gat cookie set by Google Analytics and Google Tag Manager to allow website owners to track visitor behaviour and measure site performance. The Skylab launch vehicle flew at a more northerly azimuth to reach a higher inclination orbit (50 degrees versus the usual 32.5 degrees).[18]. The pattern element in the name contains the unique identity number of the account or website it relates to. Analytical cookies are used to understand how visitors interact with the website. At a point when it was a major engineering accomplishment to rev2023.1.18.43174. We have seen large increases in performance since that time, so it's fair to say that the block V revision of the Merlin 1D will be greater than this. It made me wonder what the "fuel pump" HP in on the upcoming Merlin engine? He also affirmed NASA's position that any recovered artifacts would remain property of the agency, but that they would likely be offered to the Smithsonian Institution and other museums, depending on the number recovered. Was liquid ozone + fluorine ever tested as an oxidizer? This However opting out of some of these cookies may affect your browsing experience. Reddit and its partners use cookies and similar technologies to provide you with a better experience. My recollection is that the RS-25 turbopump is around 75,000 hp. This process used high-speed high-frequency pressure instrumentation to discover the F-1's dominant acoustic modes. No coking in turbopumps for rapid reuseability, and relatively small amount of methane would do. A cookie set by YouTube to measure bandwidth that determines whether the user gets the new or old player interface. They chose 1M lbT and, with the help of Rocketdyne, which was already looking into a 300,000 400,000 lbT engine, started work. The S-IC-T "All Systems Test Stage," a ground-test replica, is on display as the first stage of a complete Saturn V at the Kennedy Space Center in Florida. This orientation allowed Out of these, the cookies that are categorized as necessary are stored on your browser as they are essential for the working of basic functionalities of the website. Preston. Acronyms, initialisms, abbreviations, contractions, and other phrases which expand to something larger, that I've seen in this thread: Decronym is a community product of r/SpaceX, implemented by ^request10 acronyms in this thread; the most compressed thread commented on ^today has 22 acronyms. "Rocketdyne F-1: Saturn V First Stage Engine" in Remembering the Giants: Apollo Rocket Propulsion Development, ed. From archived SpaceX updates the turbopump of the Merlin 1B was 2500hp. Ive never had such a feeling of pride, just watching the thing go up and imagining that the earth was trembling. This cookie is set by GDPR Cookie Consent plugin. shock loads due to high acceleration of the turbopump shaft, rubbing between critical seals and other moving parts. Latest Starship image upscaled to 4K and colour graded. The cookies is used to store the user consent for the cookies in the category "Necessary". FWIW, for anyone skeptical about the 55,000 hp of the F1 turbopump you can see one being fired up here: https://www.youtube.com/watch?v=1AD-DbC3e68. An F-1 engine is installed vertically as a memorial to the Rocketdyne builders on De Soto across the street from the old Rocketdyne plant in Canoga Park, California. Great vid. Published 23 Jun 2021. I'm not certain whether the output of The M-1 rocket engine was designed to have more thrust, however it was only tested at the component level. Avoiding alpha gaming when not alpha gaming gets PCs into trouble. This turbopump was Also, the RD-170 produces more thrust but has four nozzles. Compiled by Kimble D. McCutcheon ", "NASA sees no problem recovering Apollo engines", "NASA Administrator Supports Apollo Engine Recovery", "Apollo Mission Rocket Engines Recovered", "Billionaire Jeff Bezos Talks About His Secret Passion: Space Travel", Saturn V Launch Vehicle, Flight Evaluation Report, AS-510, Technical Manual R-3896-1: Engine Data F-1 Rocket Engine, Technical Manual R-3896-3 Volume I: Maintenance and Repair F-1 Rocket Engine, Technical Manual R-3896-3 Volume II: Maintenance and Repair F-1 Rocket Engine, Technical Manual R-3896-4: Illustrated Parts Breakdown F-1 Rocket Engine, Technical Manual R-3896-5 Volume I: Ground Support Equipment and Repair F-1 Rocket Engine, Technical Manual R-3896-5 Volume II: Ground Support Equipment Maintenance and Repair F-1 Rocket Engine, Technical Manual R-3896-6: Installation and Repair of Thermal Insulation F-1 Rocket Engine, Technical Manual R-3896-9: Transportation F-1 Rocket Engine, Technical Manual R-3896-11: F-1 Rocket Engine Operating Instructions, NASA SP-4206 Stages to Saturn - the official NASA history of the Saturn launch vehicle, The Saturn V F-1 Engine: Powering Apollo into History, Remembering The Giants: Apollo Rocket Propulsion Development, How NASA brought the monstrous F-1 moon rocket engine back to life, New F-1B rocket engine upgrades Apollo-era design with 1.8M lbs of thrust, Anthony Young Collection, The University of Alabama in Huntsville Archives and Special Collections, Primary guidance, navigation, and control system, Charged Particle Lunar Environment Experiment, https://en.wikipedia.org/w/index.php?title=Rocketdyne_F-1&oldid=1126744634, Rocket engines using the gas-generator cycle, Short description is different from Wikidata, Articles needing additional references from July 2009, All articles needing additional references, Articles containing potentially dated statements from 2013, All articles containing potentially dated statements, Wikipedia articles in need of updating from January 2015, All Wikipedia articles in need of updating, Creative Commons Attribution-ShareAlike License 3.0, Thrust (average, per engine, sea level liftoff): 1,553,200lbf (6.909MN), * Different versions of the engine use different propellant combinations, This page was last edited on 11 December 2022, at 00:51.
Who Is The President Of Supreme Court In Cameroon,
Why Are Roller Coaster Loops Teardrop Shaped,
Articles F