• Thumbnail for Turbopump
    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...
    13 KB (1,434 words) - 19:18, 19 September 2024
  • Thumbnail for SpaceX Merlin
    engine (LMDE). Propellants are fed by a single-shaft, dual-impeller turbopump. The turbopump also provides high-pressure fluid for the hydraulic actuators,...
    52 KB (5,268 words) - 14:10, 14 August 2024
  • Thumbnail for Aerojet M-1
    nominal 1.5 million pounds force, and the designers deliberately added more turbopump capability to allow it to expand to at least 1.8 million and potentially...
    21 KB (2,386 words) - 08:04, 7 August 2024
  • Thumbnail for Rocketdyne J-2
    thrust chamber injector received the propellants under pressure from the turbopumps, then mixed them in a manner that produced the most efficient combustion...
    46 KB (5,784 words) - 16:17, 20 September 2024
  • Thumbnail for PGM-17 Thor
    to a turbopump failure. A month later, Atlas 6B also suffered a turbopump failure and the Air Force gave in and agreed to replace the turbopumps in all...
    33 KB (4,369 words) - 16:02, 14 August 2024
  • Thumbnail for Turbomolecular pump
    turbomolecular pump is a type of vacuum pump, superficially similar to a turbopump, used to obtain and maintain high vacuum. These pumps work on the principle...
    11 KB (1,587 words) - 11:05, 9 December 2023
  • Thumbnail for RS-25
    RS-25 (section Turbopumps)
    through low-pressure fuel and oxidizer turbopumps (LPFTP and LPOTP), and from there into high-pressure turbopumps (HPFTP and HPOTP). From these HPTPs the...
    106 KB (10,613 words) - 18:35, 7 September 2024
  • Thumbnail for RP-1
    likely to block fuel lines and engine passages, and wear away valves and turbopump bearings, as these are lubricated by the fuel. Slightly too-heavy or too-light...
    18 KB (2,215 words) - 13:10, 31 May 2024
  • steam was used to drive the turbopump in the German V2 rocket, and the pumps in several other rocket engines. The turbopump was used to transport fuel...
    4 KB (511 words) - 08:39, 20 August 2024
  • Thumbnail for Pump inducer
    makes the rotating speed of the turbopump rotor as high as possible. For example, the rotating speed of the oxygen turbopump of the Japanese LE-7 rocket engine...
    3 KB (281 words) - 18:03, 19 May 2022
  • Thumbnail for Staged combustion cycle
    non-stoichiometric conditions, increasing the volume of flow driving the turbopumps that feed the engine with propellant. The gas is then injected into the...
    27 KB (2,664 words) - 02:27, 2 September 2024
  • Thumbnail for RD-170
    combustion chambers, all supplied by one single-shaft, single-turbine turbopump rated at 170 MW (230,000 hp) in a staged combustion cycle. Several Soviet...
    12 KB (943 words) - 18:26, 6 September 2024
  • Thumbnail for V-2 rocket
    Both the alcohol and oxygen tanks were an aluminum-magnesium alloy. The turbopump, rotating at 4,000 rpm, forced the alcohol and oxygen into the combustion...
    97 KB (11,220 words) - 23:45, 2 September 2024
  • Thumbnail for Vulcain (rocket engine)
    liquid hydrogen turbopump. The liquid oxygen turbopump is the responsibility of Avio (Italy), and the gas turbines that power the turbopumps and the nozzle...
    16 KB (1,065 words) - 16:14, 20 September 2024
  • Thumbnail for North American X-15
    liquid oxygen as propellant, and hydrogen peroxide to drive the high-speed turbopump that delivered propellants to the engine. It could burn 15,000 pounds...
    43 KB (4,056 words) - 02:32, 11 September 2024
  • Thumbnail for Liquid-propellant rocket
    centrifugal turbopumps due to their high power and light weight, although reciprocating pumps have been employed in the past. Turbopumps are usually lightweight...
    53 KB (6,614 words) - 15:52, 29 August 2024
  • Liquid-fuel engine Propellant LOX / RP-1 Cycle Combustion tap-off Pumps Turbopump Configuration Chamber 1 Performance Thrust, vacuum 1,023 kN (230,000 lbf)...
    6 KB (297 words) - 21:36, 17 September 2024
  • Thumbnail for Atlas LV-3B
    two static engine tests and one launch (Missile 11F) fell victim to LOX turbopump explosions caused by the impeller blades rubbing against the metal casing...
    30 KB (3,755 words) - 09:20, 17 May 2024
  • Thumbnail for Fuel pump
    level sensor (the latter used for the fuel gauge). Rocket engines use a turbopump to supply the fuel and oxidizer into the combustion chamber. List of auto...
    6 KB (787 words) - 16:40, 23 April 2024
  • Thumbnail for Combustion tap-off cycle
    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...
    4 KB (399 words) - 06:29, 8 October 2022
  • Thumbnail for Sputnik 1
    one second earlier when a sensor detected overspeed of the empty RP-1 turbopump. There were 375 kg (827 lb) of LOX remaining at cutoff. At 19.9 seconds...
    79 KB (8,476 words) - 05:38, 11 September 2024
  • Thumbnail for NK-33
    oxygen-rich staged combustion cycle bipropellant rocket engines. The turbopumps require subcooled liquid oxygen (LOX) to cool the bearings. The United...
    23 KB (2,428 words) - 22:34, 20 September 2024
  • Thumbnail for Aerojet LR87
    vehicles. Composed of twin motors with separate combustion chambers and turbopump machinery, it is considered a single unit and was never flown as a single...
    16 KB (1,209 words) - 23:17, 14 July 2024
  • Thumbnail for Gemini 12
    booster. During orbital injection, the GATV engine experienced a drop in turbopump speed lasting about 2.5 seconds. After this, pump performance returned...
    18 KB (1,674 words) - 02:02, 22 July 2024
  • Thumbnail for Gas-generator cycle
    Expander cycle Pressure-fed engine Rocket engine Staged combustion cycle Turbopump "RD-107". Encyclopedia Astronautica. Archived from the original on 2014-02-09...
    5 KB (485 words) - 03:51, 10 July 2024
  • Thumbnail for Rocket propellant
    oxidizing oxidizer is introduced into a combustion chamber, typically using a turbopump to overcome the pressure. As combustion takes place, the liquid propellant...
    29 KB (3,883 words) - 23:36, 27 June 2024
  • Thumbnail for Components of jet engines
    burnt. Turbopumps are very commonly used with rockets, but ramjets and turbojets also have been known to use them. The drive gases for the turbopump is usually...
    45 KB (6,618 words) - 15:14, 7 September 2024
  • Thumbnail for Rocket
    use lightweight, low pressure tanks and typically run high-performance turbopumps to force the propellant into the combustion chamber. Some notable mass...
    107 KB (11,393 words) - 17:31, 5 September 2024
  • Thumbnail for Demonstration Rocket for Agile Cislunar Operations
    system relative to chemical engines. This drives design of the engine turbopumps and thermal management of the reactor subsystem. The committee also emphasized...
    22 KB (2,353 words) - 21:14, 13 September 2024
  • Thumbnail for SpaceX Starship
    structure itself is mostly aluminum, copper, and steel; oxidizer-side turbopumps and manifolds subject to corrosive oxygen-rich flames are made of an Inconel-like...
    174 KB (14,672 words) - 18:21, 19 September 2024