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General parameters used for constructing nose cone profiles. Given the problem of the aerodynamic design of the nose cone section of any vehicle or body meant to travel through a compressible fluid medium (such as a rocket or aircraft, missile, shell or bullet), an important problem is the determination of the nose cone geometrical shape for optimum performance.
The nose cone of an RAF Typhoon F2. A nose cone is the conically shaped forwardmost section of a rocket, guided missile or aircraft, designed to modulate oncoming airflow behaviors and minimize aerodynamic drag. Nose cones are also designed for submerged watercraft such as submarines, submersibles and torpedoes, and in high-speed land vehicles ...
A drag-reducing aerospike is a device (see nose cone design) used to reduce the forebody pressure aerodynamic drag of blunt bodies at supersonic speeds. The aerospike creates a detached shock ahead of the body. Between the shock and the forebody a zone of recirculating flow occurs which acts like a more streamlined forebody profile, reducing ...
Artist's rendering of a payload fairing being jettisoned An example of clamshell fairing of Falcon 9 during testing, 27 May 2013. A payload fairing is a nose cone used to protect a spacecraft payload against the impact of dynamic pressure and aerodynamic heating during launch through an atmosphere.
Rocket engines of upper stages perform all their operations in space and therefore in a vacuum. In order to achieve maximum efficiency for this class of engines they need high area ratios . This makes the nozzles a very sizable part of the engine, which must be completely enclosed below the nose cone of a rocket.
Later today, in what will likely be its last mission of 2019, SpaceX will attempt to recover the entire nose cone section of one of its Falcon 9 rockets. If successful and the rocket itself is ...
The rocket is designed to send up to 100 kg into low-Earth orbit, at a price of US$1 million per launch. [9] They later announced that their Executor Aerospike engine would produce 50,500 pounds-force (225 kN) of thrust at sea level and 73,800 pounds-force (328 kN) of thrust in a vacuum.
The French armament company of Matra produced three types of rocket launcher for use with the SNEB 68 mm rockets: . Matra Type 116M rocket launcher – This is lightly constructed and used as an expendable rocket launcher pod with a frangible nose cone, loaded with 19 SNEB 68mm rockets which are fired in one rippled 0.5 second salvo with a time interval of 33 milliseconds between each rocket ...