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Print/export Download as PDF; ... English: Schematic diagram of a V-2 rocket design. Own work based on: ... Usage on az.wikipedia.org
A few Soviet rocket designs, one of which was used to launch Sputnik, the first artificial satellite into orbit. Arabic بعض من إصدارات صواريخ الإطلاق السوفيتية.
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.
The design of the GTR-18A rocket is very simplistic and intended for minimal cost with the fuselage and nose cone being constructed from phenolic paper while the fins are constructed out of styrofoam. [6] [5] The fuselage and fins are joined to the nose cone by the motor tube which contains 499 grams (17.6 oz) of X-60 solid fuel propellant. [2]
A payload or second stage would have fit atop the core stage, and two detachable Space Shuttle Solid Rocket Boosters would have been mounted on the sides of the core stage as on the Shuttle. Period illustrations suggest that much larger rockets than NLS-1 were contemplated, using multiples of the NLS-1 core stage. [4]
Print/export Download as PDF; Printable version; In other projects ... Help. Pages in category "Makeyev Rocket Design Bureau" The following 13 pages are in this ...
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The fission-fragment rocket is a rocket engine design that directly harnesses hot nuclear fission products for thrust, as opposed to using a separate fluid as working mass. The design can, in theory, produce very high specific impulse while still being well within the abilities of current technologies.