Abstract

A model of safe landing capsule and ICBM multi war head transportation system for cluster type bomb attack by analysis of seed landing trajectory. Swietenia mahagoni (mahogany) seed has the uniqueness on its falling characteristics. At the time of falling, mahogany seed rotates in the axis center which is similar to the gyration of propeller towards its pivot point. The seeds look and behave like helicopter rotors. The gyration slows down the landing time whereby it is furthering the landing distance of the mahogany seeds. In this paper focused on this characteristic of the mahogany seed for real world application analysis and also the whole seed model application analysis also including some tests on the seeds.

Highlights

  • Helicopters include seeds or oneseeded fruits with a rigid or membranous wing at one end

  • Paper and seeds all follow complicated trajectories as they fall. This certain phenomenon is greatly utilized by nature; one good example can be seen in trees in their seed dispersal

  • There are a lot of tree species among them are Swetenia mahogany that have developed rather special way of dispersing seeds in the environment

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Summary

Introduction

Helicopters ( called Whirlybirds) include seeds or oneseeded fruits (samaras) with a rigid or membranous wing at one end. Paper and seeds all follow complicated trajectories as they fall. This certain phenomenon is greatly utilized by nature; one good example can be seen in trees in their seed dispersal. It is easier to use this simple structured but complex falling characteristic model for real life applications. Nowadays parasuit is used for life saving while plane accident or air strike but there are too much limitations for use. As example it needs proper eject situation for pilot to eject, proper altitude for properly bloom and a heavy hit while landing. A natural model and phenomena is analyzed for develop this technology for which the aerodynamical characteristics of mahogany seed may be useful

Structure and Seed Model Properties Analysis
Falling Phase Analysis and Trajectories
Phase 1
Phase 2
Phase 3
Phase 5
Phase 4
Overall Falling or Landing Trajectory
Total Thrust and Aerodynamic Performance Measurement
Cluster ICBM
Final Model
Safe Landing Capsule
Result & Discussion
Conclusions

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