IIIF provides researchers rich metadata and media viewing options for comparison of works across cultural heritage collections. Visit the IIIF page to learn more. With a thrust of 25 tons, the V-2 ...
Rocket combustion and heat transfer dynamics encompass a range of interlinked phenomena critical to the design and operation of modern rocket engines. The combustion process involves rapidly reacting ...
At the heart of future rocket engines lifting off to the Moon or Mars could be a 3D printed combustion chamber. Multiple NASA centers partnered with Virgin Orbit to develop and test a uniquely ...
Most aspects of a cylinder head are relatively straightforward and easily grasped. Valve size, deck thickness and combustion chamber volume are often topics of discussion and qualify the design's ...
Alliant Techsystems recently demonstrated a critical capability of its liquid oxygen (LOX)/Methane rocket engine by igniting it in a vacuum chamber. The successful ignition test was designed to ...
Blue Origin reached a key milestone in the development of the liquid-fueled BE-3 engine successfully demonstrating deep throttle, full power, long-duration and reliable restart all in a single-test ...
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