thrust chamber वाक्य
उदाहरण वाक्य
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- The test demonstrated the repeatability of the engine performance with all its sub systems like thrust chamber, gas generator, turbo pumps and control components for the full duration.
- A full-power test of the thrust chamber for Blue Origin BE-3 liquid oxygen / liquid hydrogen upper-stage rocket engine was conducted at a NASA test facility in October 2012.
- The gas then left the turbine through exhaust ducting, passed through the heat exchanger, and exhausted into the thrust chamber through a manifold directly above the fuel inlet manifold.
- ,Blue had completed more than 100 development tests of several elements of the BE-4, including the preburner and a " regeneratively-cooled thrust chamber using multiple full-scale injector elements ".
- In cooling the chamber, the fuel made a one-half pass downward through 180 tubes and was returned in a full pass up to the thrust chamber injector through 360 tubes.
- Each of the X-33's engines, which generate 205, 000 pounds of thrust, has small combustors, or thrust chambers, that fire along curved open exhaust ramps instead of through a nozzle.
- By 1933, the Soviets had successfully developed the GIRD 09 . The engine was tested on a glider, which reached a propelled altitude of 1300 feet before its thrust chamber failed.
- Each of the X-33's engines, which generate 206, 000 pounds of thrust, has small combustors, or thrust chambers, that fire across the top of open exhaust ramps instead of through a nozzle.
- Like many other liquid-fuel rocket engines, the XLR99s used regenerative cooling, in that the thrust chamber and nozzle had tubing surrounding it, through which the propellant and oxidizer passed before being burned.
- The engine, which is being developed by the Rocketdyne division of Boeing Corp ., has been plagued by development bugs, including a major problem in bonding metallic parts of the thrust chambers.
- Two PFRF tests resulted in damage to the booster engine thrust chambers, necessitating their replacement, after which 10A was taken down from the pad for a complete overhaul following the findings from 6A's flight.
- The E-D 10k nozzle had a chamber pressure of 15.5 bar ( 1.55 MPa ) delivering 10, 000 lbf ( 44.5 kN ), a cooled-thrust chamber and was tested in an altitude simulation facility.
- Officials said the engine performed well, though some erosion, in the form of pinholes, was noticed on an inside wall of a thrust chamber, a structure that replaces the bell-shaped nozzles of conventional rocket engines.
- After a delay of 1, 3, or 8 seconds, during which time fuel was circulated through the thrust chamber to condition the engine for start, the start tank discharge valve was opened to initiate turbine spin.
- The chamber was bell-shaped with a 27.5 : 1 expansion area ratio for efficient operation at altitude, and was manifold, located midway between the thrust chamber throat and the exit, at a pressure of more than.
- The major components of a cryogenic rocket engine are the combustion chamber ( thrust chamber ), pyrotechnic initiator, fuel injector, fuel cryopumps, oxidizer cryopumps, gas turbine, cryo valves, regulators, the fuel tanks, and rocket engine nozzle.
- While N-18 flew successfully from the Cape on March 21, N-21 suffered another second stage failure after having been delayed several weeks due to another episode of the first stage thrust chambers breaking off prior to launch.
- The installed Pintle Injector, unique to TRW designed liquid propulsion systems, provides improved reliability and less costly method of fuel-oxidizer impingement in the thrust chamber than conventional coaxial distributed-element injectors typically used on liquid bipropellant rocket engines.
- Some expander cycle engines may use a gas generator of some kind to start the turbine and run the engine until the heat input from the thrust chamber and nozzle skirt increases as the chamber pressure builds up.
- Soviet engineering and manufacturing processes never satisfactorily resolved combustion instability in larger RP-1 / LOX engines, so the RD-180 engine used to power the Zenit family still used four smaller thrust chambers fed by a common engine mechanism.
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