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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 ...
Oracle model rocket at apogee. During launch, the camera films downward; showing the launch pad and engine exhaust during ascent. The rocket's nose cone may be attached to the parachute in two ways; there are attachments on both ends of the nose cone. Attaching the parachute to the bottom films the parachute during descent.
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.
Estes produced a wide variety of rocket model kits, normally using paperboard tubing for the fuselage and balsa wood for fins and nose cones. Early models tended to be relatively simple in design, differing in size, number of stages and recovery method. The first kit Estes offered was the Astron Scout (Rocket Kit K-1) which sold for $ .70.
When the nose cone is placed on the rocket body, the string is placed between the nose cone and the body so that when the ejection charge of the engine expels the nose cone, the string is released causing one frame of film to be exposed. Since the rocket is not steerable, the photographer can not determine what the camera will photograph.
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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 ...