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UID:0-535@aerospace.technion.ac.il

DTSTART;TZID=Asia/Jerusalem:20141231T163000

DTEND;TZID=Asia/Jerusalem:20141231T173000

DTSTAMP:20230603T193539Z

URL:https://aerospace.technion.ac.il/events/feasibility-study-of-a-mediuml
 ong-range-ramjet-cruise-missile/

SUMMARY:Feasibility Study of a Medium/Long Range Ramjet Cruise Missile
DESCRIPTION:Lecturer:Avi Peker\n Faculty:Department of Aerospace Engineerin
 g\,\n Institute:Technion – Israel Institute of Technology\n Location:Cla
 ssroom 165\, ground floor\, Library\, Aerospace Eng.\n Zoom: \n Abstract: 
 \n Details: \n The ramjet engine is an air-breathing engine that operates 
 without the need of moving parts. This type of engine constitutes a simple
  and efficient way of propulsion. The use of a ramjet engine as a sustaine
 r of a cruise missile can be feasible because of its ability to deliver hi
 gh and constant thrust for long periods of time.\nThe present study deals 
 with the external ballistics and flight performance and also with the inte
 rnal ballistics (propulsion unit) of a supersonic cruise missile.\nThe fir
 st part involves the missile structure and aerodynamic properties\, aerody
 namic heating and it effect on the design parameters and a 3DOF trajectory
  simulation of the missile. The internal ballistics study includes the ram
 jet/solid booster engine performance analysis where thrust\, specific impu
 lse and flow mass are derived as a function of altitude and flight velocit
 y.
CATEGORIES:Seminars
LOCATION:Classroom 165\, ground floor\, Library\, Aerospace Eng.

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DTSTART:20141026T010000

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