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- combustor is designed to produce an area of low velocity airflow (Mach~0.05) where the fuel and air can be mixed and stably burnt. This area of the combustor...4 KB (525 words) - 14:09, 22 March 2013
- unmoderated, and produces more fuel than it consumes. They are said to "breed" fuel, because they produce fissionable fuel during operation because of neutron...74 KB (7,341 words) - 17:31, 16 May 2020
- providing fuel to the engine, the fuel system is also used to control propeller speeds, compressor airflow and cool lubrication oil. Fuel is usually...36 KB (5,673 words) - 06:34, 17 December 2012
- < Spacecraft docking and berthing mechanisms < User:Tony Mach/Docking Spacecraft docking and berthing mechanisms are mechanisms which are used to connect...38 KB (3,264 words) - 13:48, 2 August 2023
- drawing below. Vehicle power is provided by onboard hydrogen-oxygen fuel cells. Hydrogen fuel is breathed from the tube itself, liquid oxygen (LOX) is carried...19 KB (2,716 words) - 14:06, 2 August 2023
- Reversing Systems Final Reserve Fuel Alternate Fuel Additional Fuel Extra Fuel Taxi Fuel Contingency Fuel Trip Fuel Block Fuel AIRCRAFT WINGS BASED ON POSITION...34 KB (5,784 words) - 14:36, 24 September 2021
- use of steel was due to the heat caused by the fuel that the X-7 burnt. It ran on Hi Cal-3 zip fuel, which had a heating value of 26,500 Btu/lb. · Length:...6 KB (845 words) - 05:59, 17 April 2017
- User:Pieter1963/sandbox (section The turbojet, a short-lived jet engine with too-high fuel consumption)jet fuels in aircraft tanks vary from cold soaking at - deg F for subsonic to kinetic heating at sustained Mach 3. The cold extremes address fuel solidification...418 KB (65,198 words) - 18:59, 20 September 2024
- Canada. The main focus of the company is the development of a light multi-fuel propulsion system (DASS Engine) to power a reusable single-stage-to-orbit...17 KB (2,400 words) - 02:59, 28 July 2014
- development problems. Due to the limited internal space of the fuselage the fuel capacity was relatively small, giving the prototypes an extremely limited...3 KB (504 words) - 20:09, 6 October 2017
- could not hold much fuel. Hence all available room was adapted to the purpose of holding fuel. The flaps were even used as fuel tanks, and the landing...10 KB (1,467 words) - 23:40, 6 April 2009
- take-off. The tyre exploded, and a piece of rubber hit the fuel tank, which caused a fuel leak and led to a fire. The crew shut down engine number 2 in...9 KB (1,191 words) - 14:51, 11 June 2022
- hypersonic missiles would employ liquid cooling of the leading edges (usually the fuel en route to the engine). Aerodynamic heating is also a topic of concern in...4 KB (576 words) - 21:57, 19 January 2013
- vectoring Aerospike engine Graphite Tungsten Gimbal Gimbaled thrust Solid Fuel Solid-fuel rocket Ammonium perchlorate composite propellant Aluminium Ammonium...4 KB (439 words) - 04:17, 28 June 2016
- User:Henrickson/Aurora (aircraft) (section Fuel types)aircraft. Some of its technical descriptions are: Mach-5 capable, utilizing cryogenic hydrogen as fuel, with 4 engines (2 General Electric turbines and...36 KB (4,260 words) - 13:49, 2 August 2023
- Airbreathing jet engine Turbojet Turbofan Afterburner Scramjet Thrust specific fuel consumption Thrust reversal Turboprop Turboshaft Bypass ratio Nacelle Propeller...4 KB (362 words) - 18:40, 23 March 2017
- trailing craft to consume more fuel due to the turbulence (so called "wash") of the lead aircraft. When an emergency fuel warning was signaled in his instruments...6 KB (896 words) - 17:18, 30 July 2012
- material. From front to back, it contains the crew cabin, oxidizer tank, fuel casing, and rocket nozzle. The craft has short, wide wings, with a span of...33 KB (5,556 words) - 17:01, 21 August 2017
- understanding, in case they don’t understand other concepts like the sound barrier, machs, maybe a link to Ralph Virden. You overall have a really good draft here...24 KB (3,549 words) - 21:42, 2 May 2021
- shorter than the scramjet that requires a lengthy combustor for complete fuel-air mixing and combustion. Hence, compared to scramjet, the shcramjet has...7 KB (844 words) - 20:07, 10 July 2016
- needed for propulsion within itself—its own fuel and some form of oxidizer, commonly liquid oxygen, to burn the fuel. So the rocket engine operates independently
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