SIDDA.MANIKANTA

13761A2134

AEROSPACE Engg.

LBRCE {AP}

PRESENTATION BY

ULTRA-RAPID AIR VEHICLE

SIDDA.MANIKANTA

13761A2134

AEROSPACE Engg.

LBRCE {AP}

INTRODUCTION DESCRIPTION

ENGINESWINGSFINS

WORKING SONIC BOOM SAFETY

ZEHSTHAMMOCKS

POSSIBILIT OF PROJECT

“ULTRA-RAPID AIR VEHICLE” is recent advancement in “Aerial Locomotion.”

AIRBUS took the patent regarding development of this project.

Ultra rapid air vehicle has been dubbed the 'son of Concorde‘and would travel at four-and-a-half times the speed of sound.

It is recognized as supersonic roller coaster by

concerning the path ofthe Ultra rapid air vehicle.

Three type enginesTurbojetRocket engineRamjet

Vertical stabilizer Delta wings Fins

TURBOJET:In URAW the turbojet engines are usedin Taxiing, Takeoff and Landing. “theair vehicle’s ascension becomes near vertical.”

ROCKET:The plane would be propelled vertically byrocket engines to supersonic speeds till itreaches Cruise phase.

RAMJET:These hydrogen-powered wing mountedramjets used in cruise phase to reachthe destination.

VERTICAL STABILIZER:It is used in controlling YAW motion ofURAV.

DELTAWING:Delta wing is known for its ManeuverabilityIn this control surface is “ELEVONS”.

FINS:These pair of fins are responsible for Stabilityby maintaining center of pressure at the same point.

WORKING:

During taxiing and takeoff

Up to Sonic velocity

At Sonic velocity { M= I}

At Mach no(M)>I

SAFETY:For safety “HAMMOCKS”are provided.

GREEN TECHNOLOGY:In view of

Environmental safety ZEHST is used in URAV.

FUELS:The aircraft is envisaged to be propelled by

biofuel made from seaweed and by oxygen/hydrogen.

Reduced sonic boom results in vibroacoustic disease,a thickening of heart tissue.

Possibility of project ?