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  2. File:V-2 rocket diagram (with English labels).svg - Wikipedia

    en.wikipedia.org/wiki/File:V-2_rocket_diagram...

    This diagram was created with Inkscape …important. This diagram is translated using SVG switch elements : all translations are stored in the same file. This is a featured picture on the English language Wikipedia ( Featured pictures ) and is considered one of the finest images.

  3. Umbilical cable - Wikipedia

    en.wikipedia.org/wiki/Umbilical_cable

    For shallow water surface supply air diving, the diver's umbilical is typically a 3-part umbilical comprising a 3 ⁄ 8 inch (9.5 mm) bore breathing gas hose, 1 ⁄ 4 inch (6.4 mm) bore pneumofathometer ("pneumo") hose, and diver communications cable, which usually also serves as a lifeline strength member. The pneumo hose is open at the diver ...

  4. File:Liquid-Fuel Rocket Diagram.svg - Wikipedia

    en.wikipedia.org/wiki/File:Liquid-Fuel_Rocket...

    Liquid rocket fuel. Oxidizer. Pumps carry the fuel and oxidizer. The combustion chamber mixes and burns the two liquids. The hot exhaust is choked at the throat, which, among other things, dictates the amount of thrust produced. Exhaust exits the rocket.

  5. Rocket engine nozzle - Wikipedia

    en.wikipedia.org/wiki/Rocket_engine_nozzle

    Thrust is generated by the propulsion system of the rocket through the application of Newton's third law of motion: "For every action there is an equal and opposite reaction". A gas or working fluid is accelerated out the rear of the rocket engine nozzle, and the rocket is accelerated in the opposite direction.

  6. Piping and plumbing fitting - Wikipedia

    en.wikipedia.org/wiki/Piping_and_plumbing_fitting

    Diagram showing the construction of a typical leaded hub joint. Cast iron piping was traditionally made with one "spigot" end (plain, which was cut to length as needed) and one "socket" or "hub" end (cup-shaped). The larger-diameter hub was also called a "bell" because of its shape.

  7. Pressure-fed engine - Wikipedia

    en.wikipedia.org/wiki/Pressure-fed_engine

    Pressure-fed rocket cycle. Propellant tanks are pressurized to directly supply fuel and oxidizer to the engine, eliminating the need for turbopumps. The pressure-fed engine is a class of rocket engine designs. A separate gas supply, usually helium, pressurizes the propellant tanks to force fuel and oxidizer to the combustion chamber. To ...

  8. File:Shark finning diagram.svg - Wikipedia

    en.wikipedia.org/wiki/File:Shark_finning_diagram.svg

    You are free: to share – to copy, distribute and transmit the work; to remix – to adapt the work; Under the following conditions: attribution – You must give appropriate credit, provide a link to the license, and indicate if changes were made.

  9. File:Simplified diagram of RS-25 rocket engine(SSME) , Jan ...

    en.wikipedia.org/wiki/File:Simplified_diagram_of...

    Permission is granted to copy, distribute and/or modify this document under the terms of the GNU Free Documentation License, Version 1.2 or any later version published by the Free Software Foundation; with no Invariant Sections, no Front-Cover Texts, and no Back-Cover Texts.

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