The combustion tap-off cycle is a power cycle of a bipropellant rocketengine. The cycle takes a small portion of hot exhaust gas from the rocket engine's combustion chamber and routes it through turbopump turbines to pump fuel before being exhausted (similar to the gas-generator cycle). Since fuel is exhausted, the tap-off cycle is considered an open-cycle engine. The cycle is comparable to a gas-generator cycle engine with turbines driven by main combustion chamber exhaust rather than a separate gas generator or preburner.[1]
Diagram of the open-cycle combustion tap-off rocket cycle. A small portion of exhaust from the combustion chamber is tapped off to power the turbine(s).
The J-2S rocket engine, a cancelled engine developed by NASA, used the combustion tap-off cycle and was first successfully tested in 1969.[2]
By 2013, Blue Origin, with their New Shepard launch vehicle, had successfully flight-tested the BE-3 engine using a tap-off cycle. According to Blue Origin, the cycle is particularly suited to human spaceflight due to its simplicity, with only one combustion chamber and a less stressful engine shutdown process. However, engine startup is more complicated, and due to the hot gas fed from the main combustion chamber into the turbopumps, the turbine must be built to withstand higher-than-normal temperatures.[3] In contrast, the upper-stage variant of the BE-3, the BE-3U, uses an expander cycle to power the turbopump, and will be used on the upper stage of the New Glenn launch vehicle.[4]
The Reaver 1 engine in Firefly Alpha uses a tap-off cycle.[5] It first flew in September 2021[6] then made it to orbit on its second attempt in October 2022.[7]
^Sutton, George (November 2005). History of Liquid Propellant Rocket Engines. American Institute of Aeronautics & Astronautics. ISBN978-1563476495.
^(PDF). Defense Technical Information Center. Defense Technical Information Center. Archived from the original (PDF) on January 16, 2017.
^Norris, Guy (9 December 2013). "Blue Origin Tests New Engine". Aviation Week & Space Technology. Penton. Retrieved 3 February 2016.
^BE-3 test update, Blue Origin, 10 August 2018, accessed 15 August 2018].
^"Tour Firefly Aerospace's Factory and Test Site With Their CEO, Tom Markusic". Retrieved 12 October 2021.
^Neal, Mihir (2 September 2021). "Firefly Aerospace's maiden flight of Alpha launch vehicle ends in failure". NASASpaceFlight. Retrieved 12 October 2021.
^Trevor, Sesnic (1 October 2022). "Firefly succeeds on second Alpha flight". NASASpaceFlight.
January 06, 2023
combustion, cycle, combustion, cycle, power, cycle, bipropellant, rocket, engine, cycle, takes, small, portion, exhaust, from, rocket, engine, combustion, chamber, routes, through, turbopump, turbines, pump, fuel, before, being, exhausted, similar, generator, . The combustion tap off cycle is a power cycle of a bipropellant rocket engine The cycle takes a small portion of hot exhaust gas from the rocket engine s combustion chamber and routes it through turbopump turbines to pump fuel before being exhausted similar to the gas generator cycle Since fuel is exhausted the tap off cycle is considered an open cycle engine The cycle is comparable to a gas generator cycle engine with turbines driven by main combustion chamber exhaust rather than a separate gas generator or preburner 1 Diagram of the open cycle combustion tap off rocket cycle A small portion of exhaust from the combustion chamber is tapped off to power the turbine s The J 2S rocket engine a cancelled engine developed by NASA used the combustion tap off cycle and was first successfully tested in 1969 2 By 2013 Blue Origin with their New Shepard launch vehicle had successfully flight tested the BE 3 engine using a tap off cycle According to Blue Origin the cycle is particularly suited to human spaceflight due to its simplicity with only one combustion chamber and a less stressful engine shutdown process However engine startup is more complicated and due to the hot gas fed from the main combustion chamber into the turbopumps the turbine must be built to withstand higher than normal temperatures 3 In contrast the upper stage variant of the BE 3 the BE 3U uses an expander cycle to power the turbopump and will be used on the upper stage of the New Glenn launch vehicle 4 The Reaver 1 engine in Firefly Alpha uses a tap off cycle 5 It first flew in September 2021 6 then made it to orbit on its second attempt in October 2022 7 See also EditExpander cycle Pressure fed engine Rocket engine Staged combustion cycle Gas generator cycleReferences Edit Sutton George November 2005 History of Liquid Propellant Rocket Engines American Institute of Aeronautics amp Astronautics ISBN 978 1563476495 Altitude Developmental Testing of the J 2S Rocket Engine PDF Defense Technical Information Center Defense Technical Information Center Archived from the original PDF on January 16 2017 Norris Guy 9 December 2013 Blue Origin Tests New Engine Aviation Week amp Space Technology Penton Retrieved 3 February 2016 BE 3 test update Blue Origin 10 August 2018 accessed 15 August 2018 Tour Firefly Aerospace s Factory and Test Site With Their CEO Tom Markusic Retrieved 12 October 2021 Neal Mihir 2 September 2021 Firefly Aerospace s maiden flight of Alpha launch vehicle ends in failure NASASpaceFlight Retrieved 12 October 2021 Trevor Sesnic 1 October 2022 Firefly succeeds on second Alpha flight NASASpaceFlight Retrieved from https en wikipedia org w index php title Combustion tap off cycle amp oldid 1114778127, wikipedia, wiki, book, books, library,
