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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.
Half of a rocket thought to have been launched by North Korea washed ashore in Japan, with the other half recovered by South Korea. Japan probes suspected North Korean rocket nose cone amid ...
A major portion of the service module was taken up by propellant and the main rocket engine. Capable of multiple restarts, this engine placed the Apollo spacecraft into and out of lunar orbit, and was used for mid-course corrections between the Earth and the Moon. The service module remained attached to the command module throughout the mission.
Armadillo Aerospace designed and built more than 12 vehicles which used about 50 engine designs for over 100 rocket flights. [13] Each design had several features in common. One was the use of modern computer technologies and electronics to simplify rocket control and reduce development costs.
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 ...