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Services(Manned and unmanned vehicles):

CONCEPTUAL AND DETAILED DESIGN

AERODYNAMIC ANALYSIS AND DESIGN

STRUCTURAL ANALYSIS AND DESIGN

FABRICATION

STRUCTURAL TESTING

FLIGHT TEST

AUTOPILOT,ELECTRONIC EQUIPMENTS AND FABRICATION MATERIALS SUPPLY

Design a Close Air Support Fighter:


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It says:Dear Mr. Mahdad Emdipour, Aerospace Engineering Faculty, Amirkabir University of Technology, Your serving as an active member in Conceptual Design of Close Air Support Fighter group is appreciated by heads of university and Armed Air Forces Organization. Hope your future role in development of Aerospace science for our graceful hometown, Islamic Republic of Iran, will be effective.
And the signs belong to:
Mahmoud Mani (Aerospace Faculty Chairman)
Nader Eivaz Ghaleh jough(Vice President of Aerospace Industry Technology)
Mohammad Ali Vaziri(President of Hesa Design Group)


Mission Specifications:


  • Payload: 3ton (including 1500 ammunitions each weight 1.5lb for GAU-81A cannon).

  • Loiter: flying for 5 min at h=20000ft

  • Strafe: firing at enemies for 10 min.

  • Cruise: flying at h=20000ft , Vcruise-out=765 km/h , Vcruise-in=850 km/h



Engine:


D-30F6

One engine ,title:D-30F6 ,BYPASS:0.57 ,STATIS TRUST: 20994lb ,dry weight: 2416kg



Base Performance:


  • Full power (without afterburning) (Н=0, Мп=0, tн=15 ºС, in=1.0)

  • Thrust: 9500 Kg

  • Fuel rate: 0.72 kg/kg hr



Full power with afterburning (Н=0, Мп=0, in=1,0)


  • Thrust: 15500 Kg

  • Fuel rate: 1.9 kg / kg hr

  • Maximum flight speed: 2.83 Mach

  • Maximum turbine rotor entry temperature: 1660 K

  • Dry weight: 2416 Kg



Wing:


  • Wing span: 10.4m

  • Swing:27m^2



Weight:


  • WT.O :13ton

  • Wfuel :3.46ton

  • Wammunitions:1020kg

  • Wbomb:1980kg



(Contact me for more information)






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