Jump to content

Nose cone: Difference between revisions

From Wikipedia, the free encyclopedia
Content deleted Content added
Blanked the page
m Reverted 3 edits by 72.43.138.146 (talk) to last revision by Arado. (TW)
Line 1: Line 1:
{{For|the Transformers character|Nosecone (Transformers)}}
[[Image:titan3 centaur nose cone.jpg|thumb|A nose cone that contained one of the [[Voyager program|Voyager]] spacecraft, mounted on top of a [[Titan IIIE|Titan III]]/[[Centaur (rocket stage)|Centaur]] [[launch vehicle]].]]

[[File:aa oneworld b777-200er n791an arp.jpg|thumb|right|[[Boeing 777#777-200ER|Boeing 777-200ER]] of [[American Airlines]]. The nose cone is the most forward [[fuselage]] piece (painted white here).]]
[[File:typhoon f2 zj910 canard arp.jpg|thumb|right|The nose cone of an [[Royal Air Force|RAF]] [[Eurofighter Typhoon|Typhoon]] F2.]]

The term '''''nose cone''''' is used to refer to the forwardmost section of a [[rocket]], guided [[missile]] or [[aircraft]]. The cone is shaped to offer minimum [[Aerodynamics|aerodynamic]] resistance. Nose cones are also designed for travel in and under water and in high speed land vehicles.

==Rocket==
On a rocket vehicle it consists of a chamber or chambers in which a satellite, instruments, animals, plants, or auxiliary equipment may be carried, and an outer surface built to withstand high temperatures generated by [[aerodynamic heating]]. Much of the fundamental research related to [[hypersonic]] flight was done towards creating viable nose cone designs for the [[atmospheric reentry]] of spacecraft and [[Intercontinental ballistic missile|ICBM]] [[Multiple independently targetable reentry vehicle|reentry vehicles]].

In a [[satellite]] vehicle, the nose cone may become the satellite itself after separating from the final [[Multistage rocket|stage]] of the rocket or it may be used to shield the satellite until orbital speed is accomplished, then separating from the satellite.

==Aircraft==
On airliners the nose cone is also a [[radome]] protecting the [[weather radar]] from aerodynamic forces.

The shape of the nose cone must be chosen for minimum drag so a [[solid of revolution]] is used that gives least resistance to motion. The article on [[nose cone design]] contains possible shapes and formulas.

==Hypersonic==
Due to the extreme temperatures involved, nose cones for high-speed applications (e.g. hypersonic speeds or atmospheric reentry of [[orbit]]al vehicles) have to be made of [[refractory]] materials. [[Pyrolytic carbon]] is one choice, [[reinforced carbon-carbon]] composite or [[HRSI]] ceramics are other popular choices. Another design strategy is using [[atmospheric reentry#Ablative|ablative heat shields]], which get consumed during operation, disposing of excess heat that way. Materials used for ablative shields include, for example [[carbon phenolic]], [[polydimethylsiloxane]] [[Composite material|composite]] with [[silica]] filler and [[carbon fiber]]s, or as in of some Chinese [[Fanhui Shi Weixing|FSW]] reentry vehicles, [[oak]] [[wood]].<ref>
{{cite web
| url = http://www.fas.org/nuke/intro/missile/basics.htm
| title = Ballistic Missile Basics
| accessdate = 2008-02-03
| work = Special Weapons Primer
| publisher = Federation of American Scientists
}}</ref>

In general, the constraints and goals for atmospheric reentry conflict with those for other high speed flight applications; during reentry a high drag blunt reentry shape is frequently used, which minimises the [[heat transfer]] by creating a [[shock wave]] that stands off from the vehicle, but some very high temperature materials may permit sharper edged designs.

==Nose cone design==
{{main|Nose cone design}}
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]] or [[bullet]]), an important problem is the determination of the nose cone geometrical shape for optimum performance. For many applications, such a task requires the definition of a [[solid of revolution]] shape that experiences minimal resistance to rapid motion through such a fluid medium, which consists of elastic particles.

== See also ==
* [[Droop-nose]]
* [[Inlet cone]]

== References ==
{{reflist}}

[[Category:Rocketry]]

[[fr:Coiffe (astronautique)]]

Revision as of 12:54, 31 March 2015

A nose cone that contained one of the Voyager spacecraft, mounted on top of a Titan III/Centaur launch vehicle.
Boeing 777-200ER of American Airlines. The nose cone is the most forward fuselage piece (painted white here).
The nose cone of an RAF Typhoon F2.

The term nose cone is used to refer to the forwardmost section of a rocket, guided missile or aircraft. The cone is shaped to offer minimum aerodynamic resistance. Nose cones are also designed for travel in and under water and in high speed land vehicles.

Rocket

On a rocket vehicle it consists of a chamber or chambers in which a satellite, instruments, animals, plants, or auxiliary equipment may be carried, and an outer surface built to withstand high temperatures generated by aerodynamic heating. Much of the fundamental research related to hypersonic flight was done towards creating viable nose cone designs for the atmospheric reentry of spacecraft and ICBM reentry vehicles.

In a satellite vehicle, the nose cone may become the satellite itself after separating from the final stage of the rocket or it may be used to shield the satellite until orbital speed is accomplished, then separating from the satellite.

Aircraft

On airliners the nose cone is also a radome protecting the weather radar from aerodynamic forces.

The shape of the nose cone must be chosen for minimum drag so a solid of revolution is used that gives least resistance to motion. The article on nose cone design contains possible shapes and formulas.

Hypersonic

Due to the extreme temperatures involved, nose cones for high-speed applications (e.g. hypersonic speeds or atmospheric reentry of orbital vehicles) have to be made of refractory materials. Pyrolytic carbon is one choice, reinforced carbon-carbon composite or HRSI ceramics are other popular choices. Another design strategy is using ablative heat shields, which get consumed during operation, disposing of excess heat that way. Materials used for ablative shields include, for example carbon phenolic, polydimethylsiloxane composite with silica filler and carbon fibers, or as in of some Chinese FSW reentry vehicles, oak wood.[1]

In general, the constraints and goals for atmospheric reentry conflict with those for other high speed flight applications; during reentry a high drag blunt reentry shape is frequently used, which minimises the heat transfer by creating a shock wave that stands off from the vehicle, but some very high temperature materials may permit sharper edged designs.

Nose cone design

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 or bullet), an important problem is the determination of the nose cone geometrical shape for optimum performance. For many applications, such a task requires the definition of a solid of revolution shape that experiences minimal resistance to rapid motion through such a fluid medium, which consists of elastic particles.

See also

References

  1. ^ "Ballistic Missile Basics". Special Weapons Primer. Federation of American Scientists. Retrieved 2008-02-03.