BGM-109 Tomahawk missile aerodynamic coefficients
#1
Wink 

could you give me some website or page link to know the aerodynamic coefficients of some type of Tomahawk missile? The reason for this is i want to build a cruise missile model which need this coefficients. Thanks for you suggestion.
Reply
#2

BGM-109 Tomahawk missile aerodynamic coefficients

The Tomahawk (US /ˈtɑːməhɔːk/ or UK /ˈtɒməhɔːk/) is a long-range, all-weather, subsonic cruise missile named after the Native American axe. Introduced by McDonnell Douglas in the 1970s, it was initially designed as a medium to long-range, low-altitude missile that could be launched from a surface platform. It has been improved several times, and due to corporate divestitures and acquisitions, is now made by Raytheon. Some Tomahawks were also manufactured by General Dynamics (now Boeing Defense, Space & Security).

A cruise missile is a guided missile used against terrestrial targets, so called because the major portion of its flight path is conducted at cruise speed (i.e., approximately constant velocity). Cruise missiles are designed to deliver a large warhead over long distances with high accuracy (i.e. small circular error probability). The dynamics of cruise are a result of aerodynamic lift (force), and the equality of the thrust or propulsion forces against aerodynamic drag and as a result there is no acceleration. Modern cruise missiles are capable of travelling at supersonic or high subsonic speeds, are self-navigating, and are able to fly on a non-ballistic, extremely low-altitude trajectory. They are distinct from unmanned aerial vehicles (UAV) in several ways: the cruise missile is a single use weapon which is always sacrificed in the mission; it is not intended to provide aerial reconnaissance; and the warhead is integrated directly into the hull of the vehicle and cannot be separated.

The first cruise missiles to be deployed were the Nazi German V-1 of World War II. Advances in transistor and computer technology have contributed to self-correcting avionic and aeronautical designs that allow missiles to be guided in flight, as opposed to only at launch. These advances developed into guided missiles and guided bombs, and later into the modern cruise missile.
Reply

Important Note..!

If you are not satisfied with above reply ,..Please

ASK HERE

So that we will collect data for you and will made reply to the request....OR try below "QUICK REPLY" box to add a reply to this page
Popular Searches: aerodynamic degree, aerodynamic elite, general ppt aerodynamic ppt, aerodynamic f1 car latest seminar ppts in research paper 2015, which coefficients to use from fir1 matlab, aerodynamic ebook, aerodynamic definition for kids,

[-]
Quick Reply
Message
Type your reply to this message here.

Image Verification
Please enter the text contained within the image into the text box below it. This process is used to prevent automated spam bots.
Image Verification
(case insensitive)

Possibly Related Threads...
Thread Author Replies Views Last Post
Wink missile guidance seminars report pdf 1 574 13-04-2016, 11:13 AM
Last Post: dhanabhagya
  adaptive missile guidance using gps abstract 1 548 04-04-2016, 12:15 PM
Last Post: dhanabhagya
  missile guidance system ppt 1 565 15-03-2016, 02:36 PM
Last Post: seminar report asees
  Adaptive Missile Guidance Using GPS gagz89 1 1,754 29-08-2011, 10:22 AM
Last Post: seminar addict
  Missile Guidance System vishala.gavi 4 3,245 30-06-2011, 11:33 AM
Last Post: smart paper boy
  Missile Guidance System tejasj 3 3,674 14-01-2011, 09:10 PM
Last Post: summer project pal
  aerodynamic performance of aerospace vehicle sheetal patnaik 1 1,535 22-09-2010, 12:40 PM
Last Post: project report helper
  adaptive missile guidance using gps pujitha 1 2,780 18-03-2010, 06:52 PM
Last Post: seminar-avatar
  guided missile technology sachin89tendulkar 1 2,158 18-03-2010, 06:52 PM
Last Post: seminar-avatar
  missile guidance ec36707 1 1,547 18-03-2010, 06:52 PM
Last Post: seminar-avatar

Forum Jump: