• Saturday, January 18, 2020

Iranian military engine development news and updates

Discussion in 'Iranian Defence Forum' started by Rukarl, Aug 29, 2016.

  1. Mithridates

    Mithridates BANNED

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    this is an awesome achievement, a single example of these engines can support an anti ship missile with ~500 kg weight and 150-250 km range (depending on it's fuel consumption).
     
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  2. AmirPatriot

    AmirPatriot SENIOR MEMBER

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    You called it.
     
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  3. Mithridates

    Mithridates BANNED

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    825380_219.jpg 2620179.jpg
    ramjet3.jpg

    seems like they only showed us the flame holder part. damn i mentioned rim-8 as an example only but it seems like the goal is some thing like that.:flame::flame:
     
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  4. PeeD

    PeeD FULL MEMBER

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    It's the whole engine in exploded display.

    The cost of a ram-jet propulsion is lower than the Noor's mini-jet Toloue.

    Seems like we will see the Noor/Ghadr/Ghadir being replaced by a ram-jet supersonic missile that may cost less than the Noor while having supersonic speed.

    I hope to see the Tolue based missiles evolve to a YJ-18/Klub like mini-jet missile with a solid rocket kill-stage. Cost of it would be more than the Ghadir but range would be much higher than a ram-jet AshM.

    Ram-jet powered AshM would have a range of between 100-300km
    Mini-jet killstage missile would have 250-600km range

    Ram-jet has a cost benefit and a superior reaction time which is important for over the horizon targeting/ISR.

    I hope for a simple solution and not a very expensive high-end solution like the Bhramos/Yakhont.
     
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  5. Draco.IMF

    Draco.IMF FULL MEMBER

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    Sharif University Aerospace Research Research Exhibition:

    -TJ-HP1 turbo jet engine
    - Micro turbine MGT-03
    -Ramjet engine

    [​IMG]
    [​IMG]
    [​IMG]
    [​IMG]
     
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  6. sahureka2

    sahureka2 FULL MEMBER

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    [QUOTE = "Draco.IMF, post: 11940750, membro: 166252"] Mostra di ricerca sulla ricerca aerospaziale dell'Università Sharif:
    ........

    [​IMG][/CITAZIONE]

    [​IMG]
     
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  7. skyshadow

    skyshadow SENIOR MEMBER

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    [​IMG]



    this small turbojet produces 1650N or 371lbs of thrust.
     
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  8. mohsen

    mohsen SENIOR MEMBER

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  9. sahureka2

    sahureka2 FULL MEMBER

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    looking at this model of V / STOL aircraft, I give an interpretation of myself, the engines shown in green rotate to pass from vertical to horizontal flight, here I attach an original image and the one modified by me with rotated engines for horizontal flight

    [​IMG]
     
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  10. skyshadow

    skyshadow SENIOR MEMBER

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    good job, what do you think about that, it can have 2 or 4 TJ-HP1 turbo jet engines for take off and landing and get it to speed then it can have one RJ-HP1 Ramjet engine, if so then this thing can easily reach mach 3.


    Iran is testing a jet powered passenger plane with capacity of 75 people so that it can be a test bed for passenger plane with capacity of 150 people, that is a good news
     
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  11. skyshadow

    skyshadow SENIOR MEMBER

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    [​IMG]

    [​IMG]

    [​IMG]
     
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  12. Mithridates

    Mithridates BANNED

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    comparing to Czech build tj-100 it's maximum thrust output improved but it's SFC is a little bad with 1.26 lb/lbf coefficient. this means for one hour non stop maximum out put thrust it consumes 50 kg more fuel.
    i assume it's cheaper than tj-100 and that's actually good.
     
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  13. Ich

    Ich FULL MEMBER

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    The TJ-HP1 would be nice to build some Coanda Aerodyne.

    Edit:

    For example to replace groundbased tanks and their disadvantages. Just build Coanda Aerodyne with graphene armor (the one the chinese experiment with) on the down side and a gun (or laser) on top.
     
    Last edited: Dec 24, 2019
  14. Hack-Hook

    Hack-Hook ELITE MEMBER

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    and how much power that laser is supposed to need
     
  15. TheImmortal

    TheImmortal SENIOR MEMBER

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    Excuse me are you saying building a tank that can fire a laser so powerful it eliminates other tanks and blows holes in buildings?

    Did you just walk out of a Star Wars movie sir?